© 2017 jorge israel medinaufdcimages.uflib.ufl.edu/uf/e0/05/10/20/00001/medina_j.pdf ·...
TRANSCRIPT
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SHINING LIGHT ON THE EXCITED STATE DYNAMICS OF MEROCYANINE-540: AN APPLICATIONS OF PUMP-PROBE TWO-DIMENSIONAL SPECTROSCOPY
By
JORGE ISRAEL MEDINA
A DISSERTATION PRESENTED TO THE GRADUATE SCHOOL OF THE UNIVERSITY OF FLORIDA IN PARTIAL FULFILLMENT
OF THE REQUIREMENTS FOR THE DEGREE OF DOCTOR OF PHILOSOPHY
UNIVERSITY OF FLORIDA
2017
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© 2017 Jorge Israel Medina
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To my parents, whose personal sacrifices and support allowed me to grow into the person I am—the days you went hungry so I could eat, worked late to provide
opportunities for me, and nurtured me after you got back from work despite being exhausted were not in vain.
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ACKNOWLEDGMENTS
I thank my advisor Professor Valeria D. Kleiman for having the patience to mold
me into a scientist. She taught me the difference between being an expert at an
experimental method (skilled technician) and a scientist. My committee also helped by
burning me down so I could rise stronger from the ashes with their help (though that
was tough on me).
I also wish to acknowledge my family, who were there for me the whole way
cheering me on and supporting me when things got hard and I wanted to quit. My
brothers especially motivated me to not quit, because I didn’t want to disappoint them–
being the middle child is hard.
There are many people who made this possible: educators who believed in me
and pressured me to apply myself; administrators who refused to suspend or expulse
me from school despite my many actions that warranted such responses, because they
saw the potential I had if I only took education seriously; mentors who guided me to
paths that are hidden to those without a guide; and friends and partners who helped me
grow as a person.
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TABLE OF CONTENTS page
ACKNOWLEDGMENTS .................................................................................................. 4
LIST OF TABLES ............................................................................................................ 7
LIST OF FIGURES .......................................................................................................... 8
LIST OF ABBREVIATIONS ........................................................................................... 13
ABSTRACT ................................................................................................................... 14
CHAPTER
1 INTRODUCTION .................................................................................................... 15
Background ............................................................................................................. 18
What is Coherence? ......................................................................................... 18 Phase ......................................................................................................... 20 Ultrafast optical pulses ............................................................................... 21
Coherent Mixing On A Detector ........................................................................ 25 Photoisomerization ........................................................................................... 27
Triplets and electro-vibrational coupling ..................................................... 28 Ultrafast photoisomer formation ................................................................. 31
Ultrafast Optical Pulses .................................................................................... 32
Pulse characterization ................................................................................ 32
Controlling ultrafast pulses ......................................................................... 37
2 TWO-DIMENSIONAL SPECTROSCOPY ............................................................... 40
History of Two-Dimensional Spectroscopy ............................................................. 40
Diagrammatic Perturbation Theory ......................................................................... 41 Pump-Probe Geometry Two-Dimensional Spectroscopy ........................................ 47 Experimental Introduction ....................................................................................... 52
Two Pump Pulses ............................................................................................ 54 Noncollinear optical parametric amplifier ................................................... 54 Pulse shaping ............................................................................................ 58
One Probe Pulse .............................................................................................. 60
Broadband Detector ......................................................................................... 61 Making Raw Data Meaningful ................................................................................. 62
Optical 2D-S Pump-Probe Spectroscopy is a Differential Spectroscopy .......... 63
A Slice of Pump-Probe 2D-S Data Corresponds to a TA experiment ............... 64
3 IMPLEMENTATION AND TROUBLESHOOTING .................................................. 73
NOPA Generation ................................................................................................... 74
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Pulse Shaping ......................................................................................................... 78 Tilted 4-f Compressor ....................................................................................... 78
Phase and Amplitude Control Using SLM-640 ................................................. 88 Pump pulse compression ........................................................................... 89 Double pulses ............................................................................................ 97
Broadband Seed/Probe Pulse ................................................................................ 99 Pump-Probe Overlap ............................................................................................ 101
Sample Holder ...................................................................................................... 101 Measuring Signal .................................................................................................. 102
Instrument Control .......................................................................................... 103 Data Collection ............................................................................................... 103 Improving Signal-to-Noise .............................................................................. 105
Data Processing and Management ....................................................................... 108
Expectation Versus Reality ................................................................................... 109
4 MEROCYANINE-540 ............................................................................................ 111
Overlapping Signals .............................................................................................. 112
Method .................................................................................................................. 113 Results .................................................................................................................. 116
Steady-State ................................................................................................... 116
Long Lived Isomer .......................................................................................... 119 Two-Dimensional Spectroscopy ..................................................................... 122
Early time 2D-S ........................................................................................ 124 Later time 2D-S ........................................................................................ 125
Transient Absorption ...................................................................................... 128
SVD / MCR-ALS ...................................................................................... 129
Time evolution .......................................................................................... 133 Discussion ............................................................................................................ 135
Ultrafast Formation of Cis-isomer Spectral Signature .................................... 136
Triplet State .................................................................................................... 138
5 CONCLUSION ...................................................................................................... 140
Merocyanine-540 Excited State Kinetics ............................................................... 142
Zwitterion Evidence?............................................................................................. 146
APPENDIX: CONSTRAINING SVD ........................................................................ 148
LIST OF REFERENCES ............................................................................................. 153
BIOGRAPHICAL SKETCH .......................................................................................... 157
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LIST OF TABLES
Table page 2-1 List of optics used in the NOPA. ......................................................................... 71
4-1 Lifetimes and amplitude percentages of SVD/MCR-ALS components of MC540. ............................................................................................................. 135
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LIST OF FIGURES
Figure 1-1 Merocyanine-540 chemical structure .................................................................. 15
1-2 Selective staining of leukemia cells by MC540 results in emission in the dark field, with no emission from healthy cells ............................................................ 17
1-3 Cosine oscillation over time that restarts after an interruption ............................ 19
1-4 Cosine oscillation over time with points at different phase. ................................ 21
1-5 Damped (decaying) cosine oscillation with a phase of 𝜋/2. ............................... 21
1-6 Phase dependence on wave mixing and illustration of phase of a pulse ............ 22
1-7 Carbon bond isomerization represented by both a simple free rotor potential and a more complicated model for a restricted rotor. ......................................... 29
1-8 Isomerization of stilbene induced by photo absorption with corresponding fluorescence quantum yield. ............................................................................... 29
1-9 Spin-Orbital mixing leading to forbidden intersystem crossing. .......................... 30
1-10 Franck-Condon overlap between two vibrational wave functions, can couple electronic states as IC, or optical transitions ...................................................... 30
1-11 Wave-packet dynamics involved in ultrafast formation of retinal rhodopsin isomerization involving a conical intersection ..................................................... 31
1-12 Frequency-Resolved Optical Gating (FROG) diagram ....................................... 33
1-13 Linear chirp of frequency components result in a pulse that appears to sweep frequencies ......................................................................................................... 34
1-14 Optical path length difference for two wavelengths in a dispersive medium ....... 36
1-15 Chromatic dispersion of two wavelengths because of travel in a dispersive medium ............................................................................................................... 36
1-16 Co-propagation of two different wavelengths inside a medium can be achieved by adding an external angle to the propagation of the beams. ............ 36
1-17 Simplified illustration of coherent mixing for OPG and OPA ............................... 38
2-1 Time assignment of the 4-wave interaction given as a difference in time between pulses. .................................................................................................. 43
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2-2 Single ket side electric field interaction represented by DPT .............................. 43
2-3 Interactions with two electric fields represented by DPT. ................................... 44
2-4 Three-wave interaction represented by DPT. ..................................................... 44
2-5 Three-wave interaction with third order response represented by DPT. ............. 45
2-6 Four non-degenerate four-wave mixing paths for a two-level system represented by DPT. .......................................................................................... 45
2-7 A ket side response is the complex conjugates of the bra side response ........... 46
2-8 Illustration of four-wave mixing in the pump-probe geometry and the corresponding third order response signal directions ......................................... 48
2-9 Three level system with two consecutive bra interactions in the same direction represented by DPT. ............................................................................ 48
2-10 Four-wave mixing with the first two fields not having the same magnitude ........ 49
2-11 Example of four-wave mixing where the system changes states between two field interactions depicted by DPT. ..................................................................... 51
2-12 Simplified diagram of a pump-probe geometry experimental setup. ................... 52
2-13 Depiction of angles involved in NOPA phase matching ...................................... 55
2-14 NOPA spectrum dependence as a function of phase matching angle in BBO ... 55
2-15 Comparison of NOPA spectrum generated with anamorphic focusing and spherical focusing ............................................................................................... 57
2-16 Optimized spectrum of the NOPA with an output energy of 2.0 𝜇J/pulse. .......... 58
2-17 Illustration of how individually controlling SLM pixels for a pulse in the Fourier plane can alter the phase and amplitude ............................................................ 59
2-18 Tilted folded 4-f compressor diagram. ................................................................ 60
2-19 Typical white light spectrum generated in sapphire with different fluence .......... 61
2-20 Simplified caricature of 2D-S data to explain on-diagonal and off-diagonal signals. ............................................................................................................... 63
2-21 Raw 2D-S data for DASPI scanning 𝜏 at constant 𝑇 = 30 𝑓𝑠 .............................. 65
2-22 Raw 2D-S data for DASPI scanning 𝑇 and constant 𝜏 ........................................ 66
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2-23 Processed 2D-S data for DASPI at two different 𝑇 values shown in Δ𝑇𝑟𝑎𝑛𝑠𝑚𝑖𝑠𝑠𝑖𝑜𝑛 ................................................................................................... 67
2-24 Processed 2D-S data for DASPI at two different 𝑇 values shown in
Δ𝐴𝑏𝑠𝑜𝑟𝑝𝑡𝑖𝑜𝑛. ...................................................................................................... 67
2-25 Published TA DASPI data .................................................................................. 68
2-26 A slice of pump-probe 2D-S data for a given excitation wavelength correspond to an equivalent TA experiment at the same excitation wavelength ......................................................................................................... 70
2-27 NOPA schematic ................................................................................................ 72
3-1 Simplified diagram of a pump-probe geometry experimental setup. ................... 73
3-2 Some typical NOPA spectrum achievable day-to-day with energies between 1.5 to 1.8 𝜇J/pulse. ............................................................................................. 74
3-3 Spatial chirp from anamorphic focusing NOPA generation is the result of a large sweep of phase matching angles inside the crystal ................................... 76
3-4 Spatial chirp of NOPA beam measured by imaging first order diffraction on a CCD .................................................................................................................... 77
3-5 Simplified illustration of pulse shaping ................................................................ 78
3-6 Tilted folded 4-f compressor design .................................................................... 79
3-7 Spatial aberrations introduced by the SLM-640 when a cylindrical mirror is used .................................................................................................................... 82
3-8 Spectral bandwidth of the pump pulse allowed through the SLM-640 array, with the 4-f compressor design used .................................................................. 82
3-9 Phase matching bandwidth for SFG between NOPA beam and 800 nm beam at various phase matching angles for 100 𝜇𝑚 thick BBO ................................... 84
3-10 X-FROG traces of the NOPA pulse + 800 nm generated piecewise at different BBO angles .......................................................................................... 86
3-11 Simple illustration to explain how we know the SLM-640 adds positive dispersion from an X-FROG Trace. .................................................................... 87
3-12 Simple illustration of why temporal chirp in a white light probe leads to blue TA signals arriving before red signals in time. .................................................... 87
3-13 Crosscorrelation of Pump pulse + 800 nm pulse before and after a compression mask obtained with a GA using SFG in BBO is applied ................ 90
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3-14 Phase matching acceptance bandwidth of KDP compared with BBO at a single crystal phase matching angle ................................................................... 91
3-15 X-FROG and cross correlation of pump + 800 nm pulse before and after compression mask obtained with a GA using SFG in KDP is applied ................ 93
3-16 Mixing compression mask can allow for pulse with better temporal profile than that achievable directly ............................................................................... 95
3-17 X-FROG and crosscorrelation of pump pulse + 800 nm pulse before and after compression mask obtained with a GA using two-photon absorption is applied ................................................................................................................ 96
3-18 Interferogram generated by generating pulse pairs with the SLM-640 to generate a convolution spectrum ........................................................................ 97
3-19 Difference in intensity of a pulse pair measured by X-FROG because of SLM array leakage ...................................................................................................... 99
3-20 Typical white light spectrum generated in sapphire with different pump fluence ................................................................................................................ 99
3-21 Effects of truncating data and Hamming windows on the resulting FFT ........... 104
3-22 Effect of collecting unneeded data past the signal decay on the FFT signal-to-noise ............................................................................................................. 105
3-23 Phase cycling data ........................................................................................... 106
4-1 Chemical structure of Merocyanine-540 in trans-isomer configuration ............. 111
4-2 Spectral signature of long lived transients ........................................................ 113
4-3 Steady state spectra collected for MC540 in methanol ..................................... 117
4-4 Excitation Spectrum of MC540 in methanol ...................................................... 118
4-5 Dilution study of MC540 absorption prepared in atmospherically wet methanol ........................................................................................................... 119
4-6 Transient signal detected before time-zero when the sample is not refreshed between pump pulses ....................................................................................... 120
4-7 Transient signal observed before “time-zero” when adequately refreshing sample between consecutive excitation pulses ................................................ 121
4-8 Solvent flow difference between home build flow cell and commercial flow cell used ........................................................................................................... 122
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4-9 2D-S signal for MC540 at 𝑇 = 0.3 ps ................................................................ 124
4-10 Snap shots of the time evolution of the 2D-S signal of MC540 in methanol at early times ........................................................................................................ 126
4-11 2D-S data for later times of MC540 in methanol ............................................... 127
4-12 TA data collected for MC540 in methanol with excitation at 480 nm ................ 128
4-13 Singular Value Decomposition values of TA data for MC540 in methanol excited at 555 nm ............................................................................................. 129
4-14 Spectral components and spectra from MCR-ALS for TA data collected at three different excitation wavelengths .............................................................. 131
4-15 Residuals from TA data excited at 555 nm fit using the SVD/MCR-ASL results ............................................................................................................... 132
4-16 Composition of spectral signitures of SVD/MCR-ASL components .................. 134
4-17 Normalized cis-isomer component amplitude kinetics ...................................... 138
5-1 Transient data for a model merocyanine which shows spectral signatures like those observed for merocyanine-540 ............................................................... 143
5-2 VB structure used to assign transition from work by Haas on the MCM system .............................................................................................................. 144
5-3 Reproduction of plots shown in Figure 4-15. .................................................... 145
A-1 Example of a decaying exponential signal with noise ....................................... 151
A-2 Two unconstrained fits of MC540 TA data that fit the data well, but have no physical meaning .............................................................................................. 152
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LIST OF ABBREVIATIONS
BBO 𝛽-Barium Borate
BOA Born-Oppenheimer approximation
CCD Charged Coupled Device
DPT Diagrammatic Perturbation Theory
FWHM Full-Width and Half-Max
FROG Frequency Resolved Optical Gating
GA Genetic Algorithm
KDP Potassium Dihydrogen Phosphate
MCR-ALS Multivariate Curve Resolution Alternating Least Square
MC540 Merocyanine-540
NOPA Noncolinear Optical Parametric Amplifier
SFG Sum-Frequency Generation
SHG Second Harmonic Generation
SLM Spatial Light Modulator
SVD Single Value Decomposition
TA Transient Absorption
2D-S Two-Dimensional Spectroscopy
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Abstract of Dissertation Presented to the Graduate School
of the University of Florida in Partial Fulfillment of the Requirements for the Degree of Doctor of Philosophy
SHINING LIGHT ON THE EXCITED STATE DYNAMICS OF MEROCYANINE-540: AN
APPLICATIONS OF PUMP-PROBE TWO-DIMENSIONAL SPECTROSCOPY
By
Jorge Israel Medina
May 2017
Chair: Valeria D. Kleiman Major: Chemistry
The anionic molecular dye Merocyanine-540 is soluble in a variety of solvents;
has an environment dependent fluorescent yield making it a good molecular probe; and
forms an isomer and triplet upon visible light absorption. MC540 has been extensively
studied because it selectively binds to leukemia cells, killing the cells after irradiation
with visible light. Though many of its properties are well known, the excited state
dynamics that lead to isomerization and triplet formation are still not well understood
and there are conflicting conclusions in the literature. We present 2D-visible
spectroscopy as a new tool to resolve the dependence of the excited state dynamics on
excitation wavelength. Combined with Transient Absorption to help understand the
kinetics of selected excitation wavelengths.
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CHAPTER 1 INTRODUCTION
“Character is as important in science as it is in any other field” David Hahn
Figure 1-1. Merocyanine-540 chemical structure. When in solution the 𝑁𝑎+dissociates leaving the molecule with both polar and non-polar character.
Merocyanine-540 (MC540), shown in Figure 1-1, is a molecular dye which has
perplexed scientist since discovering the dye selectively binds to leukemia cells in the
late 1970’s.1 Figure 1-2 shows that MC540 bound to leukemia cells is emissive in the
dark field, while healthy cells are dark. Soon after discovering selective binding to
leukemic cells, it was discovered that cells stained with MC540 and irradiated with
visible light would die; though leukemia cells die at orders of magnitude higher (~0.01%
survival) compared to healthy cells (>80% survival).2 This discovery led to a boom of
basic science research to try to understand the excited state dynamics of MC540 to be
able to understand the mechanism of the highly selective cytotoxicity. It was established
that MC540 forms a triplet state, and an unstable isomer after absorbing visible light.3
Plenty of debate in the literature exists to the mechanism involved in killing leukemia
cells, some arguing that the triplet formation kills leukemia through formation of singlet
oxygen, and others claiming it’s the isomerization process which kills leukemia by
disturbing the cell membrane. But no experiment proves conclusively which process
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kills leukemia, because it is hard to generate the triplet and isomer independently with
the irradiation sources used for in-vitro experiments.
In 1986, work by Clakson et al. conclusively showed that MC540 is not a viable
treatment method for leukemia—MC540 does significant harm to healthy cells.4 The
percent recovery (compares the growth of a cell line exposed to drug, and one not
exposed to drug) of healthy cells exposed to MC540 is ~20% recovery at a dose which
would kill leukemia cells with more selectivity than healthy cells. For comparison, a high
dose of a chemotherapy drug used to treat leukemia, vincristine, has ~80% recovery for
healthy cells and ~25% recovery for leukemic cells.5 MC540 does more harm to healthy
cells than a high dose of chemotherapy does to cancer cells—interest in MC540 on the
medical application side quickly diminished after discovering MC540 would not cure
leukemia. However, MC540 remained an interesting system for basic science, a
predictive model for the excited state dynamics of MC540 remains elusive despite
intense study on the molecule. Each time a new experimental method is applied to
MC540 something new is discovered that violates the previously held predictive model,
meaning our models are wrong—a model that can’t predict experimental results is
wrong.
Complicating things further than the complexity of the molecules excited state
dynamics is the loss of primary referencing. Many things about MC540 are assumed in
the literature because they are referenced so frequently making it difficult to distinguish
between what is known (direct experimental evidence), what is suspected (calculations
and model systems), and what is speculative.
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Figure 1-2. Selective staining of leukemia cells by MC540 results in emission in the dark field, with no emission from healthy cells. A) Leukemic mouse cells seen by microscopy and in the dark-field, B) healthy human cells in the top panel, showing no emission and leukemic cells in the bottom panel showing emission. Part A, reprinted from, Cell, Vol. 13, J. Valinsky, T. Easton, E. Reich, Merocyanine 540 as
a Fluorescent Probe of Membranes: Selective Staining of Leukemic and Immature Hemopoietin Cells, 487-499, Copyright (1978), with permission from Elsevier. Part B, reprinted from Cancer Research, Copyright (1986), Vol. 46, 4892-4895, J. Atzpodien, S. Gulati, B. Clarkson, Comparison of the Cytotoxic Effects of Merocyanine-540 on Leukemic Cells and Normal Human Marrow, with permission from AACR.
Dark-Field Microscopy (emission)
Microscopy (absorption)
Mouse Cells (leukemic)
Human Cells (healthy)
Human Cells (leukemic)
A
B
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MC540 remains untested to the relativly new technique of two-dimensional
optical spectroscopy, until now. We shed light on the excited state dynamics of MC540
using a newly built instrument able to apply the new experimental technique in a difficult
to access region of the visible spectrum. As history of MC540 predicted, the new
findings cannot be explained by the current models for the excited state dynamics of
MC540, meaning we need a new predictive model. More work besides my own will be
needed to understand the excited state dynamics of MC540, but this work expands our
understanding of a complex system.
Background
Some terminology and concepts are needed for the reader to be able to follow
the experimental methods used to study MC540 and the results. Transient absorption
(TA) is a basic experimental method now in the mainstream, so it will not be introduced
in detail, however, an excellent review article6 is available if more than a refresher is
needed. An understanding of quantum mechanics and its use with first-order light-
matter interaction perturbation theory is also assumed—when a certain result is needed,
it will be reviewed, but not derived.
What is Coherence?
When I introduce my work, “what is coherence?” is often the first question asked.
Coherence is a ‘catch-all’ term in science, so it is difficult to pin down and explain,
because it represents many concepts. Coherence is maintaining the ability to predict the
state of an oscillating system at some future time. For example, Figure 1-3 shows the
oscillation of simple cosine wave that gets interrupted and restarts after an interruption.
All waves are coherent but the state of the oscillation as shown only has coherence
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between interruptions, because if the interruptions are random there is no way to predict
the future state of the oscillation once it has been interrupted. If the interruptions follow
some statistical distribution, such as Poisson distribution for collisions, then the mean
time between collisions is the “coherence time” of the system. There are many others
forms of coherence and all are called some form of “coherence”. Coherence can be lost
by interruptions(collisions), damping (decay), destructive interference (mixing many
waves such that it becomes impossible to predict the future evolution) and any other
process that prevents future prediction of the system.
Figure 1-3. Cosine oscillation over time that restarts after an interruption (dashed line).
An example of incoherent and coherent fields in spectroscopy is emission of
photons from an excited state. In spontaneous emission, a single emitted photon is
coherent but photons are emitted at random times and with random phase (phase
explained next section), making it impossible to predict the state of oscillation of each
photon. When a spontaneous emission signal is measured the mixture of the many
emitted photons with random time evolution destructively interfere and the signal has no
clear “wave-nature”. Stimulated emission on the other hand is coherent because the
emission is not spontaneous (random), and follows a clear dependence on the phase of
the perturbing field, the emitted photons will follow the time dependence of the field
stimulating the emission. Lasers are based on stimulated emission and are therefore
coherent. Lamps (fluorescent bulbs and incandescent bulbs) work on spontaneous
emission and are not coherent.
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The working definition used in optical spectroscopy to determine whether a signal
from a system is coherent or incoherent is phase dependence of the signal on the
perturbing field (laser). Phase is explained next.
Phase
The phase of a wave is the instantaneous position of a point (specified time) in
the time evolution of a wave. Figure 1-4 shows a cosine evolving in time, the blue point
is at phase zero, the red point is at phase 3𝜋
2, the green point is at phase 2𝜋, and the
purple point is at phase 6𝜋; each defined by what the value of cosine would yield the
current position of the wave. From Fourier theory, a cosine oscillation has no phase
(imaginary) component, while a sine, which is just a cosine with phase 𝜋/2, has no real
component, and entirely in the phase (imaginary) component. The “time-zero” of a wave
is arbitrary in experiments thus the “phase” of the wave is assigned as the deviation
from a simple cosine oscillation that starts at zero. Figure 1-5 shows a damped
(decaying) cosine oscillation. The phase of the decaying cosine signal is 𝜋/2, because
at “time-zero” the oscillation is a cosine with phase 𝜋/2. In NMR, the start of the
measurement and the start of the signal which is being measured often don’t coincide,
so the phase of signal is an “error” because the start time of the signal is unknown. In
two-dimensional optical spectroscopy (introduced in Chapter 2), the start time of the
measurement is well-defined, and starts at the same time as the signal which is
measured, so when the phase of the signal is not zero it is not a phase error, but the
actual phase of the signal being measured. It will be shown in Chapter 3, that the phase
of the signal can be controlled with the phase of the laser pulse generating the signal,
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thus two-dimensional optical spectroscopy is a coherent spectroscopy because the
signal is phase dependent.
Figure 1-4. Cosine oscillation over time with points at different phase.
Figure 1-5. Damped (decaying) cosine oscillation with a phase of 𝜋/2.
Ultrafast optical pulses
The Fourier transform of a Gaussian is a Gaussian, so a Gaussian pulse in the
time domain requires a Gaussian distribution of frequencies. Light waves are composed
of photons and photons only have a single frequency, so a pulse in the time-domain
cannot be composed of a single frequency photon. A pulse of coherent light (laser
pulse) is achieved by the constructive interference between many different “colors”
(frequencies in the optical range of the electromagnetic spectrum are visible to human
eyes and seen as distinct colors). To ensure constructive interference the phase of
individual frequency components must be fixed (phase-locked), because random phase
or phase drift result in destructive interference. Figure 1-6 shows the result of
superposition of many different frequencies (top panels) resulting in a pulse of light
…
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(bottom panel), represented by the electric field E(t). Superposition of waves with phase
zero generate a phase zero pulse (red colors), and 𝜋/2 phase waves superimpose for a
pulse with phase 𝜋/2 (blue colors).
Figure 1-6. Phase dependence on wave mixing and illustration of phase of a pulse. The red pulse has the mixing waves locked at zero phase, and the blue wave has the mixing waves locked at 𝜋/2 phase. This is only a caricature because many more frequencies than the ones shown would need to mix to make the pulse displayed.
The duration, Δ𝑡 (full width at half maximum), of a Gaussian laser pulse is limited
by the equation 1-1,
Δ𝑡 ⋅ Δ𝜈 ≥ 0.441 (1-1)
where Δ𝜈 is the bandwidth of frequencies (full width at half maximum), and the constant
0.441 is the result for Gaussian pulses when the Δ represents full width at half
maximum and accounting for the Heisenberg uncertainty principle,
Δ𝑡 ⋅ Δ𝐸 ≥ ℏ (1-2)
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where Δ𝐸 is the uncertainty in energy (not the electric field). A transform-limited
Gaussian pulse is defined as a pulse which satisfies Δ𝑡 ⋅ Δ𝜈 = 0.441, implying that it is
not possible to make the pulse shorter in time without more spectral bandwidth.
When dealing with laser pulses, it is inconvenient to keep track of all the
individual frequencies which compose the pulses electric field, instead an effective
representation is made, given by equations 1-3,
�� (𝑡) = 𝐴 (𝑡) ⋅ cos(𝜔𝑡 + 𝜙(𝑡)) (1-3)
where the electric field, �� (𝑡), of an electromagnetic wave is represented with a carrier
frequency oscillation, 𝜔, inside a pulse envelope, 𝐴 (𝑡), and phase of 𝜙(𝑡) which can
have time dependence. An approximation can simplify the math whenever an electric
field or its response will be measured. A cosine can be rewritten in the form given by
equation 1-4,
cos(𝜔𝑡 + 𝜙) = ℜ[𝑒𝑖(𝜔𝑡+𝜙)] (1-4)
by instead representing the field oscillations without the requirement of only considering
the “real” component, given by equation 1-5,
cos(𝜔𝑡 + 𝜙) ≅ 𝑒𝑖(𝜔𝑡+𝜙) (1-5)
The approximation given by equation 1-5 greatly simplifies math involving an
electric field treated semi-classically as a transverse wave. The field can thus be written
as equation 1-6,
�� (𝑡) = 𝐴 ′(𝑡)𝑒𝑖(𝜔𝑡+𝜙) (1-6)
where 𝐴 ′ is a constant multiple of 𝐴 in equation 1-3 that accounts for the difference in an
amplitude measured by a detector, when ignoring detector response (discussed later).
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This approximation is valid in most circumstances involving optical frequency
pulses because the wavelength of an optical pulse is much longer than a typical
absorbing molecule, ~100’s of nm compared to 0.1-1 nm (meaning the field amplitude
can be treated as constant at any single time of the interaction ignoring the oscillations
of the field), and detectors have a response time much longer than the period of optical
pulses, and can thus not resolve the oscillations of the field. By representing the
oscillations of a field as equation 1-6, the field no longer oscillates in intensity but moves
in and out of the real plane and the phase plane (implying intensity does not oscillate),
given by the equation 1-7 and equation 1-8,
ei(ωt+ϕ) = cos(𝜔𝑡 + 𝜙) + 𝑖 ⋅ sin(𝜔𝑡 + 𝜙) (1-7)
|ei(ωt+ϕ)| = 1 (1-8)
Intensity is given by the magnitude of the field convoluted with the response of the
detector squared, given in equation 1-9,
𝐼(𝑡) = |�� (𝑡) ∗ 𝑅(𝑡)|2 (1-9)
where 𝐼(𝑡) is the measured intensity of the field and 𝑅 is the response of the detector.
Thus, the intensity will not oscillate and have no phase dependence if the field is
represented using the approximation giving in equation 1-6 and the detector response is
ignored; or if the response time of the detector is too slow to resolve the real form of the
electric field giving by equation 1-3 (fast optical detectors have ~1 nanoseconds
response time and optical frequencies have a period of ~2 femtoseconds meaning an
optical detector cannot detect the oscillations of the field).
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Coherent Mixing On A Detector
The intensity of two pulses, �� 1 and �� 2, mixing on an intensity detector is phase
dependent even if the detector cannot resolve the phase or oscillations of each field
independently. Ignoring the response time of the detector by using the assumption in
equation 1-6, the phase dependence of mixing fields on a detector is derived in
equations 1-10 through 1-16:
𝐼(𝑡) = |�� 1(𝑡) + �� 2(𝑡)|2 (1-10)
𝐼 = (�� 1 + �� 2) ⋅ (�� 1 + �� 2)∗ (1-11)
𝐼 = �� 1 ⋅ �� 1∗ + �� 1 ⋅ �� 2
∗ + �� 2 ⋅ �� 1∗ + �� 2�� 2
∗ (1-12)
𝐼 = 𝐴 12 + �� 1 ⋅ �� 2
∗ + �� 1∗ ⋅ �� 2 + 𝐴 2
2 (1-13)
To clean things up and end at an important result, the two fields will be assumed
to be in the same direction, losing the need for vector notation.
𝐼(𝑡) = 𝐴12 + 𝐴1𝑒
𝑖(𝜔1𝑡+𝜙1) ⋅ 𝐴2𝑒−𝑖(𝜔2𝑡+𝜙2) + 𝐴1𝑒
−𝑖(𝜔1𝑡+𝜙1) ⋅ 𝐴2𝑒𝑖(𝜔2𝑡+𝜙2) + 𝐴2
2 (1-14)
𝐼(𝑡) = 𝐴12 + 𝐴2
2 + 2 𝐴1 𝐴2 cos((𝜔1 − 𝜔2)𝑡 + 𝜙1 − 𝜙2) (1-15)
𝐼(𝑡) = 𝐴1(𝑡)2 + 𝐴2(𝑡)
2 + 2 𝐴1(𝑡) 𝐴2(𝑡) cos(𝛥𝜔12𝑡 + 𝛥𝜙12) (1-16)
Equation 1-16 explains how two pulses can interfere on a detector depending on their
phase and frequency difference. The interference term is important because it allows a
field with an 𝐴2 too small to be measured directly, to be measured indirectly by mixing
with a field that can be measured and looking at the cross term. When the two pulses
are the same, the cross term is called a homodyne. When the two pulses are different,
the cross term is called a heterodyne. A Michelson interferometer is an example of
using the homodyne to measure an ultrafast pulse; an optical detector is too slow to
resolve each pulses time profile, but by scanning one pulse in time over the other, the
cross term shows a time dependence proportional to the field temporal profile. Using the
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approximation given in equation 1-6 to derive equation 1-16, the full signal measured by
a Michelson interferometer is not reproduced. The fringe oscillations in an interferogram
are a result of a cos((𝜔1 + 𝜔2)𝑡 + 𝜙1 + 𝜙2) term that is lost by assuming the field is not
oscillating, because the 𝑒−𝑖(𝜔𝑡+𝜙) term of a cosine is ignored. Working out equation 1-9
using the full form of the cosine given by the Euler formula,
cos(x) =1
2[𝑒𝑖𝑥 + 𝑒−𝑖𝑥]
(1-17)
and including the detector response will fully reproduce the signal generated by the
coherent mixing of waves on a detector, but the math gets complicated because the
convolution with the response of the detector cannot be ignored. The full form of the
cosine is rarely used when explaining theory and instead it is mentioned that there is an
extra term lost by approximation.
Heterodyne detection is important, because a 2D-S signal is the result of a third-
order weak perturbation, which is too weak to be measured directly by a detector. But
by mixing the signal with another pulse on the detector, the cross term can have enough
intensity to be measured.
In quantum mechanics, the wave function is a complex wave, that oscillates in
and out of the real and imaginary plane, the amplitude is both real and complex, but an
electric field component of an electromagnetic wave is purely real. Representation of an
electric field as a complex wave simplifies the math in light matter interactions and when
the magnitude of the wave is measured, but having a non-zero complex component
does not represents the real wave.
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Photoisomerization
Isomerization is a large field in chemistry and biology, being an important part of
many mechanisms. We will limit our discussion to photoisomerization process, where a
molecule can be transformed to another configuration through the absorption of light.
The term ‘trans’ and ‘cis’ are often used to describe two configurations of a molecule
with isomerization along a carbon double bond. Trans corresponds to when the two
adjacent bonds are on opposite sides, and cis corresponds to when the two adjacent
bonds are on the same side. When a carbon double bond is not involved or if the
convention of adjacent bonds becomes ambiguous, the terms used to describe two
isomers are, Z and E. Given by the first letters for the German words together
(zusammen) and opposite (entgegen). Cahn–Ingold–Prelog priority rules are used to
determine which moieties have priority, if the two highest priority parts are on the same
side, the molecule is a Z-isomer.
Isomerization along a carbon double bond is very relevant in chemistry and has
been extensively studied. The text book7 explanation of photoisomerization along a
carbon double bond are shown in Figure 1-7, where a double-well exists in the ground
state (Ψ), and an excited state (Ψ∗) couples to both wells. The photoisomerization of
stilbene is shown in Figure 1-8, directly under Figure 1-7B, which shows the potential
surfaces to help explain the behavior observed in the fluorescent quantum yield. Trans-
stilbene must overcome a steric hindrance, shown as an activation energy, 𝐸𝑎 to form
the cis-isomer, resulting in a potential well that can trap some of the population and
result in emission from the excited state. The height of the barrier which needs to be
overcome determines the rates and yields of isomerization. Cis-stilbene has a torque
applied by steric interactions resulting in no potential well in initial excited state, thus no
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emission is observed because the rate of isomerization is significantly faster than
emission.
When two electronic potential energy surfaces get close in energy such as that
shown in figure 1-7 where the ground state electronic surface reaches the excited state
electronic surface, there is a breakdown of the Born-Oppenheimer approximation.
Born-Oppenheimer approximation (BOA) allows the electronic (electron) and
vibrational (nuclei) component of a wave function to be treated independently because
nuclear motion is so slow compared to electronic motions, thus they are not coupled
significantly. However, when two different electronic wave function get close in energy,
the vibrations of one electronic surface can couple to another electronic surface
vibrations—breakdown of the Born-Oppenheimer approximation. Breakdown of the
BOA for surface crossings and conical intersections are the text book example for
intersystem crossing (ISC) to a triplet state from a singlet state, and internal conversion
(IC).
Triplets and electro-vibrational coupling
Intersystem crossing (ISC) and internal conversion (IC) are terms used when two
electronic states are coupled through vibrational modes—breakdown of the Born-
Oppenheimer approximation (BOA). When the transition is forbidden (i.e. spin-
forbidden), the coupling is termed ISC. Allowed transition are termed IC.
Singlet, doublet, triplet… states are named because of the signal generated by
NMR/EPR. A singlet electronic state, will make a single signal peak, and a doublet state
will form two signal peaks, and so on. The number of peaks is related to the spin of the
system, a system with all the spins paired will only give one transition frequency after
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splitting from a strong magnetic field. A triplet state has two electrons with unpaired
spin, the splitting after a strong magnetic field will have 3 transition signals.
Figure 1-7. Carbon bond isomerization represented by both a simple free rotor potential and a more complicated model for a restricted rotor. A) Free rotation potential, B) restricted rotation potential showing that the initial excited state must overcome a barrier to reach the twisted geometry. Figure adapted from Turro,
N. J.; Scaiano, J. C.; Ramamurthy, V. Principles of Molecular Photochemistry: An Introduction University Science Books: California, 2008; pp 289 & 341. Reproduced with permission from University Science Books, all rights reserved.
Figure 1-8. Isomerization of stilbene induced by photo absorption with corresponding fluorescence quantum yield.
The spin of a system is a conserved quantity when the BOA holds; when it
breaks down, forbidden electronic transitions which violate conservation of spin can
occur. A vibration can couple two electronic state states, that don’t have overlap in a
stationary frame (electronic orbitals not accounting for vibrations), called spin-orbital
mixing. A simple example for spin orbital mixing from a vibration is shown in Figure 1-9.
A B
ℏ𝜔
trans cis
ℏ𝜔
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Figure 1-9. Spin-Orbital mixing leading to forbidden intersystem crossing. Figure adapted
from Turro, N. J.; Scaiano, J. C.; Ramamurthy, V. Principles of Molecular Photochemistry: An Introduction University Science Books: California, 2008; pp 287. Reproduced with permission from University Science Books, all rights reserved.
Figure 1-10. Franck-Condon overlap between two vibrational wave functions, can couple electronic states as IC, or optical transitions. A) F-C overlap from surface crossing resulting in IC between 𝑆2 ↔ 𝑆1, B) F-C effect on Absorption spectrum. Figures adapted Turro, N. J.; Scaiano, J. C.; Ramamurthy, V. Principles of Molecular
Photochemistry: An Introduction University Science Books: California, 2008; pp 129 & 292. Reproduced with permission from University Science Books, all rights reserved.
When vibrations can couple two electronic transition in the stationary frame, IC
occurs because of wave function overlap. The overlap between two stationary
vibrational wave functions is called Franck-Condon overlap (F-C). Figure 1-10A shows
how F-C overlap can couple vibrational modes from surface crossings and effect optical
transition between two electronic surfaces. If the energy separation between two
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surfaces is accessible through thermal perturbations, IC will occur if the F-C factor is
large enough for the transition to be allowed. At room temperature kT ~ 200 𝑐𝑚−1, is on
the same order of low energy bending and twisting modes. If the energy gap is larger
than that accessible by thermal fluctuations, a perturbing field is required to couple two
electronic surfaces, as either a resonant absorption or emission photon. The effect of F-
C on absorption spectrum is shown in Figure 1-10B.
Ultrafast photoisomer formation
Surface crossings and conical intersections can lead to ultrafast isomerization
processes, such as that observed for retinal rhodopsin.8 Using transient absorption
(TA), the ultrafast formation of retinal rhodopsin was observed to occur within 200 fs by
tracking the stimulated emission and photoinduced absorption as a function of time.
Figure 1-11 depicts how the formation of the isomer was tracked over time by TA.
Starting at the initial excited state (star 1), reaching a conical intersection (star 2) and
then changing isomer state (star 3).
Figure 1-11. Wave-packet dynamics involved in ultrafast formation of retinal rhodopsin isomerization involving a conical intersection. Reprinted by permission from Macmillan
Publishers Ltd. [Nature] Polli, D.; Altoè, P.; Weingart, O.; Spillane, K. M.; Manzoni, C.; Brida, D.; Tomasello, G.; Orlandi, G.; Kukura, P.; Mathies, R. A.; Garavelli, M.; Cerullo, G. Conical intersection dynamics of the primary photoisomerization event in vision Nature 2010, 467, 440-443, copyright (2010).
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A short time after the work on retinal rhodopsin, theoretical predictions that the
conical intersection separation could be tuned with solvent polarity were experimentally
verified on a simple merocyanine molecule.9 Tuning a conical intersection to have a
smaller energy gap results in less thermal fluctuations needed to initiate IC or ISC,
making the transition rate higher.
Ultrafast Optical Pulses
Ultrafast optical spectroscopy relies on being able to produce ultrafast optical
pulses with the desired properties. Electronics to characterize the pulses directly don’t
exist, so other methods to indirectly characterize the pulse are used, such as coherent
wave mixing on a detector. Once a pulse is characterized, it can be controlled: changing
its time, changing its frequency, and changing its phase. Being able to control ultrafast
pulse is critical, because very few ultrafast lasers exists to preform experiments outside
a narrow range of wavelengths available by Ti:sapphire and Fiber lasers.
Pulse characterization
The standard pulse characterization method used in ultrafast optical
spectroscopy was pioneered by Trebino10, called Frequency-Resolved Optics Gating
(FROG). FROG is a spectrally-resolved autocorrelation; an autocorrelator would only
give the intensity of a pulse as a function of time, while FROG provides intensity and the
corresponding frequency. A diagram of the simplest form of FROG can be found in
Figure 1-12.
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Figure 1-12. Frequency-Resolved Optical Gating (FROG) diagram. Figure adapted from
Frequency-Resolved Optical Gating: The Measurement of Ultrashort Laser Pulses, Chapter 4, 2000, pp. 65, Rick Trebino, copyright (2000). With permission of Springer Nature.
When dealing with broadband optical pulses, it is important to know where each
frequency is in time, not just the shape of the intensity autocorrelation. The critical
importance of this will be demonstrated in Chapter 3 when dealing with a complex
optical pulse. Sometimes, it is impossible or impractical to generate a non-linear signal
for FROG using autocorrelation, so instead an unknown pulse is mixed with a known
pulse to characterize the unknown pulse in a crosscorrelation FROG (X-FROG). X-
FROG can give essential information about the chirp of a pulse, while an autocorrelation
FROG will only show that there is chirp without being able to determine the exact
direction of the chirp.
Pulse temporal chirp is coined from the sound a bird makes when it chirps, an
audio frequency sweep from high to low frequencies or low to high. Linear chirp in
optical pulses is a result of individual frequencies not travelling together with the same
phase. Pulses shown in Figure 1-6, all have the same phase for each frequency
component, as is shown with the dashed black line. A chirped pulses frequency
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components would look like Figure 1-13A and result in a temporal pulse profile with the
lowered frequencies arriving first, as shown in Figure 1-13B.
Figure 1-13. Linear chirp of frequency components result in a pulse that appears to sweep frequencies. A) frequencies with a negative linear dependence in phase as a function of frequency. Linear chirp is linear in phase, not linear in time as shown with the dashed-red guide line. B) Resulting chirp of an ultrafast pulse with frequency components with negative chirp. This figure is only an illustration, the amount of frequencies needed to make the pulse shown in B is significantly higher than those shown in A.
Chromatic dispersion: All materials, including air, have a wavelength
dependent refractive index that changes the phase of a frequency after traveling
through the medium. An example is depicted in Figure 1-14. The index of refraction,
𝑛(𝜆), of a material is an indication of the phase velocity of light in the medium compared
with that in a vacuum, given by equation 1-18.
n(𝜆) =𝑐
𝑣𝑚(𝜆) (1-18)
The speed of light, c, is a conserved quantity, so when light travels in a medium
at a slower velocity, it travels a longer optical path length (OPL) to conserve the speed
A
B
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of light, given by equations 1-19. OPL makes chromatic dispersion easier to
understand, as depicted in Figure 1-15 and Figure 1-16.
OPL = n(λ) ∗ 𝐿𝑚 (1-19)
𝐿𝑚 represents the distance traveled inside a dispersive medium. OPL can be
understood as the effective distance traveled, allowing time of arrival to be calculated
using the speed of light. Figure 1-14 depicts how two different wavelengths would travel
different effective paths inside a medium. Each arriving at the end at separate times, if
they started together. The blue wave traveled 50% longer time inside the medium.
Figure 1-15 depicts chromatic dispersion and how Snell’s Law works. Since different
wavelength travel at different speeds in a material, the blue wavelength spends more
effective distance in the medium, so the two colors will leave the medium spatially
separated. Transparent lenses rely on differences in OPL to focus beams of the same
color, and will not focus all colors at the same focal point, because each color
experiences a different OPL. Optical lenses have the focus given in terms of 633 nm, it
is only the focal point for 633 nm, redder wavelengths will focus farther away than 633
nm, and bluer wavelengths will focus closer than 633 nm. When the focus position of
many colors is critical, curved mirrors are required to avoid the problem of chromatic
dispersion.
Figure 1-15 shows that two different wavelengths entering a medium propagating
in the same direction will separate spatially inside of a medium. However, by tuning an
external angle between the two wavelengths as the beams enter the medium, the
beams can be made to co-propagate inside the medium, as seen in Figure 1-16. The
external angle dependence and ability for two wavelengths to co-propagate in space
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inside a medium is important for non-collinear optical parametric generation, which will
be introduced in Chapter 2.
Figure 1-14. Optical path length difference for two wavelengths in a dispersive medium. Wavelength and OPL are color coded.
Figure 1-15. Chromatic dispersion of two wavelengths because of travel in a dispersive medium. Blue and Red waves and material match those in Figure 1-14. Black lines are all parallel and show that the direction of propagation is conserved.
Figure 1-16. Co-propagation of two different wavelengths inside a medium can be achieved by adding an external angle to the propagation of the beams.
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Controlling ultrafast pulses
Many wave mixing methods exist to generate desired wavelengths from one
fundamental laser pulse. The most common methods are optical parametric generation
(OPG), and optical parametric amplification (OPA). The underlying theory is complex
because it relies on non-linear response of mediums, so it will not be introduced in detail
(any optical ultrafast spectroscopy book covers OPA and OPG in detail because it is the
first step a laser pulse experiences in most experiments). The basic concepts of OPG
and OPA are illustrated in Figure 1-17, as well as the naming convention for pump,
idler, signal/seed. The range of wavelengths that can be generated by wave mixing is
governed by the conservation of energy and momentum, given by equation 1-20, where
|�� | =2𝜋
𝜆. Mixing can be simplified to only show the wavelength dependence, ignoring the
direction of propagation as equation 1-21.
k pump = �� 𝑠𝑖𝑔𝑛𝑎𝑙 + �� 𝑖𝑑𝑙𝑒𝑟 (1-20)
1
λpump=
1
𝜆𝑠𝑖𝑔𝑛𝑎𝑙/𝑠𝑒𝑒𝑑+
1
𝜆𝑖𝑑𝑙𝑒𝑟
(1-21)
Equation 1-20 is manipulatable, for example, �� 𝑝𝑢𝑚𝑝 − �� 𝑠𝑖𝑔𝑛𝑎𝑙 = �� 𝑖𝑑𝑙𝑒𝑟 is called
down conversion because two pulses mix to make a lower frequency pulse. If the idler
and signal are the same, the processed is called second harmonic generation. Equation
1-20 written as �� 𝑠𝑖𝑔𝑛𝑎𝑙 + �� 𝑖𝑑𝑙𝑒𝑟 = �� 𝑝𝑢𝑚𝑝 is called up conversion because two pulses mix
to make a higher frequency pulse. Pulses generated from an OPA/OPG processes can
be used for a different OPA/OPG processes, for example an 800 nm wave can be
doubled to 400 nm, then 800 nm and the generated 400 nm can be mixed in another
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crystal to form 266 nm. OPA/OPG is a result of non-linear response of a medium, thus
will not occur in vacuum.
Figure 1-17. Simplified illustration of coherent mixing for OPG and OPA. OPG generates new wavelengths from one. OPA is amplification of one pulse at the expense of another, resulting in a third pulse needed to conserve momentum. Pump, signal/seed, and idler are named according the wavelength of the pulses.
For OPG/OPA processes to occur, the mixing waves must overlap in space and
time to coherently mix. The chromatic dispersion of materials make overlap in space
and time quite challenging to overcome because every material has a wavelength
dependent index of refraction, which means two pulses of different wavelengths will
separate in time as they travel in a medium.
Non-linear Material
Non-linear Material
pump
signal
idler
pump
seed
idler
signal
OPG
OPA
𝜆𝑝𝑢𝑚𝑝 < 𝜆𝑠𝑖𝑔𝑛𝑎𝑙/𝑠𝑒𝑒𝑑 < 𝜆𝑖𝑑𝑙𝑒𝑟
𝜔𝑝𝑢𝑚𝑝 > 𝜔𝑠𝑖𝑔𝑛𝑎𝑙/𝑠𝑒𝑒𝑑 > 𝜔𝑖𝑑𝑙𝑒𝑟
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Birefringent crystals have two index of refractions, an ordinary and
extraordinary, each with different values as a function of wavelength; the crystal
structure determines if a crystal will be birefringent. If a condition exists where both
wavelengths can experience the same effective index of refraction, one wavelength can
experience the ordinary index of refraction, and the other wavelength extraordinary
index of refraction, both waves can co-propagate in the material. When two
wavelengths experience the same effective speed in a material it is called the phase
matching condition. Materials which have negligible difference in index of refraction as a
function of wavelength, like air for optical pulses, are always phase matched. Indeed
OPA/OPG processes will occur in air at high enough intensities.11 OPA/OPG efficiency
is a function of the polarizability of the material, so the polarizability of a material is just
as important as the ability to phase match. Air can phase match easily, but has very low
polarizability making it a poor non-linear material. The most common nonlinear crystal
for optical pulses is 𝛽 −barium-borate (BBO) because it has a decent phase matching
range in the optical range and has a high polarizability.12
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CHAPTER 2 TWO-DIMENSIONAL SPECTROSCOPY
"Let's change the world, one femtosecond pulse at a time." Russ Bowers
The objective of this chapter is to introduce the reader to the key concept of Two-
Dimensional Spectroscopy (2D-S); included here is an introduction of the theory, how to
perform an experiment, analyze the data, and what can be learned from pump-probe
geometry 2D-S. This chapter will not go into detail on the theory or formalism and will
instead focus on diagrammatic perturbation theory (DPT) which is simpler to
understand. From DPT, the experimental method will be introduced, followed by data to
explain how the equations from the theory relate to the signals observed. For a detailed
understanding of the underlying quantum mechanics and formalism, there is an
introductory book by Hamm and Zanni13, and a literature review by Cho14.
History of Two-Dimensional Spectroscopy
Two-Dimensional Spectroscopy (2D-S) was first introduced in pulsed NMR
experiments.15 Warren was the first to apply the concepts of 2D-S to optical pulses
using femtosecond spectroscopy16, but the method was limited because shaping optical
pulses is very difficult compared to shaping RF pulses. The fastest electronics work in
the 100’s of GHz range and can thus modulate pulses for EPR (~95 GHz and lower)
and NMR (~1 GHz and lower). An optical pulse has a frequency in the THz range which
is too high for modulation through electronic shapers. The high frequency of optical
pulses also leads to phase instability because a difference of a ~100 nm optical path
(thermal fluctuations of materials or air density changes) is on the order of the optical
wavelength. Originally, coherent optical pulse pairs were made through diffractive
optics17, but the method was plagued by phase distortions because each pulse would
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travel separate locations in space. The problems of phase distortions were solved by
taking advantage of optical pulse shapers to turn one coherent pulse into two;18 by
having the pulses pair travel the exact same path, fluctuations in optical path would be
eliminated because both pulses would experience the same net phase change and 2D-
S signal is only dependent on the difference in phase of the two pulses. A short time
after, it was shown that optical 2D-S could extract more information by using broadband
detection pulses, so that experiments were not limited to detecting the range that was
excited.19 Finally, 2D-S was put into the mainstream by showing how to turn a TA
experimental setup into 2D-S using a pulse shaper.20 The current direction of 2D-S is
ultra-broadband excitation and detection, in the attempt to collect the most amount of
information possible.
Diagrammatic Perturbation Theory
Diagrammatic Perturbation Theory (DPT) allows multi-photon spectroscopy
theory to be more easily understood by using Feynman diagrams built from time-
dependent density matrix perturbation theory to keep track of each photon interaction
and the overall response of the system. DPT assumes the perturbing fields are weak
allowing to only consider the first order perturbation, thus a multi-photon interaction
response of a system can be built using linear response theory for each perturbing field.
To build the theory, some basic formalism needs to be introduced.
|𝛹𝑖(𝑡)⟩ = ∑𝑐𝑘(𝑡)|𝑘⟩
𝑘
(2-1)
𝜌(𝑡) ≡ |𝛹(𝑡)⟩⟨𝛹(𝑡)| (2-2)
𝜌𝑛𝑚(𝑡) ≡ ⟨𝑛|𝛹(𝑡)⟩⟨𝛹(𝑡)| 𝑚⟩ = 𝑐𝑛(𝑡) ⋅ 𝑐𝑚∗ (𝑡) (2-3)
∴ 𝜌𝑙𝑙(𝑡) = |𝑐𝑙(𝑡) |2= P𝑙(𝑡)
(2-4)
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where 𝜌(𝑡) is the projection operator into density matrix notation and |Ψi(𝑡)⟩ is the time
dependent wave function in an eigen basis for a single “ith” molecule of an ensemble.
𝜌𝑛𝑚 is the corresponding matrix element, (n,m). The matrix elements are products of the
time dependent amplitudes and their complex conjugates, 𝑐𝑛(𝑡)𝑐𝑚∗ (𝑡), of the eigen
states. Thus, in the eigen basis, the diagonal elements of 𝜌, 𝜌𝑙𝑙 provides the probability
of measuring the corresponding state 𝑙 as a function of time, P𝑙(𝑡). Representing the
state of the system with 𝜌 is convenient if the initial condition of the system, |Ψ(𝑡)⟩, is
known, because 𝜌 can be evolved in time using time-dependent perturbation theory as
matrix elements. Using perturbation theory to treat the light-matter interaction of a two-
level system is a simple way to introduce DPT because it captures the essentials
needed to understand 2D-S. To start, we need to know the initial state of the system; for
electronic transitions in the visible regime the lowest electronic state can be assumed.
This assumption can be understood by considering the Boltzmann distribution at room
temperature for a two-level system separated by an energy gap of ~550 nm (green
light); the excited state is negligibly populated. In the following, |𝐴⟩ will represents the
ground state, and |𝐵⟩ the excited state for the two-level system.
2D-S is a four-wave mixing process, in which each electric field, 𝐸n , is resonant
with the A↔B transition and therefore couples states A & B. When the electric field 𝐸𝑛
interacts with the system, the system will have population transition to the other state.
Each of the 4 waves occur at separate times, and it is convenient to look at the
difference in time between the pulses, instead of absolute time. The naming convention
for the time differences is shown in Figure 2-1
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Figure 2-1. Time assignment of the 4-wave interaction given as a difference in time between pulses.
In DPT, electric field interactions are represented with arrows. An arrow inward,
represents an absorption event, and an arrow outward represents a stimulated emission
event. Arrows on the left side are ket side interactions, and arrows on the right are bra
side interactions. Figure 2-2 shows an absorption event on the ket side.
Figure 2-2. Single ket side electric field interaction represented by DPT. An arrow in represents absorption, and the arrow on the left side represents a ket side interaction. Dashed lines represent breaks in time-evolution of the system because of a perturbing electric field (one of the four waves in a 4-wave mixing process).
The dashed line in Figure 2-2 represents the interaction of the system with the
first field, 𝐸1. Because the difference in time between pulses is used, time starts at the
first interaction. Time evolves upward in a DPT figure, so for the single interaction
shown in Figure 2-2, the system evolves in time in the state |𝐵⟩⟨𝐴| with the time
evolution given by equation 2-5, until the next field arrives.
𝑅(3) ∝ eiωBA𝜏 ⋅ e−Γ𝜏 (2-5)
where 𝑅(3) is the third-order system response contribution from the first field. 𝜔𝐴𝐵 is the
frequency of the transition between state A and B, and Γ is the dephasing/decoherence
rate of |𝐵⟩⟨𝐴|. These mixed states, correspond to off diagonal elements of the density
0 Time
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matrix representing a superposition of eigen states |𝐴⟩ and |𝐵⟩, and are called
coherences because there is a phase dependence in their time evolution, evolving with
𝜏. Coherence in the system will evolve until the next interaction with an electric field.
Figure 2-3. Interactions with two electric fields represented by DPT.
A two-wave interaction would be depicted by Figure 2-3. The second electric field
shown puts the system into state |𝐵⟩⟨𝐵|. This eigen state is referred to as a population
state, because if it was measured, it would directly give the probability of being in state
B and it corresponds to on-diagonal elements of the density matrix. The population
states evolve in time as a decay with time 𝑇, given by equation 2-6.
where 𝜏𝐵 is the life-time of state |𝐵⟩⟨𝐵|, a term accounting for both spontaneous
emission and non-radiative relaxation processes. The third interaction in a two-level
system shown so far can only be stimulated emission, because there isn’t a higher level
to absorb into and would be represented as Figure 2-4.
Figure 2-4. Three-wave interaction represented by DPT.
The third wave is stimulated emission and the system goes into another coherent
state, |𝐴⟩⟨𝐵|, which evolves with the equation 2-7.
𝑅(3) ∝ 𝑒−𝑇𝜏𝐵
(2-6)
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𝑅(3) ∝ 𝑒−𝑖𝜔𝐵𝐴𝑡 ⋅ 𝑒−Γt (2-7)
where, 𝑡 is the time that passes between the third pulse and when the final signal is
measured. Γ for |𝐴⟩⟨𝐵| is the same as for equation 2-5 because the superposition
losses coherence at the same rate. The fourth and final wave, is the response that is
detected in 2D-S. The system must end in a population state because the response is
an observable signal. So, the system must end in |𝐴⟩⟨𝐴| or |𝐵⟩⟨𝐵|. The combination of
the 3 waves and the final wave are represented in Figure 2-5.
The system response, 𝑅(3) shown in figure 2-5, is a third-order response of three
perturbations generating the response. The final response can thus be written as a
product of factors of equation 2-5, 2-6, and 2-7, of 𝑅(3) as equation 2-8:
Figure 2-5. Three-wave interaction with third order response represented by DPT.
𝑅(3) ∝ 𝑒𝑖𝜔𝐵𝐴𝜏 ⋅ 𝑒−Γ𝜏 ⋅ 𝑒−𝑇𝜏𝐵 ⋅ 𝑒−𝑖𝜔𝐵𝐴𝑡 ⋅ 𝑒−Γ𝑡
(2-8)
Figure 2-6. Four non-degenerate four-wave mixing paths for a two-level system represented by DPT.
For a two-level system, there are four non-equivalent ways leading to four-wave
mixing response, represented in Figure 2-6. All responses will be simultaneously
A B C D
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generated and the observable signal from the system would be given by a combination
of all the cases, given by equation 2-9.
𝑆(3) ∝ ∑[𝑅𝑖(3)
− 𝑅𝑖∗(3)
]
𝑖
(2-9)
The third order signal, 𝑆(3) is made up of each of the non-degenerate system
responses and their complex conjugate. Third order responses that are emitted on the
ket side, one example shown in Figure 2-7, are the complex conjugates of one of the
bra side responses shown in Figure 2-6A, and are thus accounted for in equation 2-8.
Showing DPT figures with the response on the ket or bra side is a matter of preference.
The subtraction of the response and complex conjugate is the result of using the density
matrix representation of time evolution, because the observable is the trace of the 𝜌(𝑡);
the math involved to go from qualitative DPT figures to the final form of the observable
signal in a quantitative form is beyond the scope of this work, but is explained clearly in
an open access lecture by Tokmakoff.21
Figure 2-7. A ket side response is the complex conjugates of the bra side response.
This diagram is 𝑹𝟏∗ (3)
from Figure 2-6A.
Something ignored up to here is the dependence of the direction of propagation
of the four fields. From conservation of momentum we can get the direction of the
emitted signal from equation 2-10.
�� 𝑠𝑖𝑔 = 𝑘1 + 𝑘2
+ 𝑘3 (2-10)
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were, �� 𝑖 is the wave vector with magnitude |�� | =𝜔
𝑐, 𝜔 being the angular frequency of the
field, and c the speed of light. Because of the rotating wave approximation used in
perturbation theory, the true field direction is lost; a pulse incident from the left is
indistinguishable from a pulse incident from the right. Instead, a pulse that interacts with
the ket side has a positive k direction, and a pulse that interacts with the bra side has a
negative k direction. This can be understood by the field direction, given by 𝑒𝑖�� ⋅𝑥 , a bra
side interaction is the complex conjugate of the field, so 𝑒−𝑖�� ⋅𝑥 represents a field from
the opposite direction even though the actual field direction is the same for both a ket
and bra interaction. A stimulated emission event is the complex conjugate of an
absorption, so an arrow out on the ket side is negative, and an arrow out on the bra side
is positive. Tokmakoff explains the math behind the field vector direction in an open
access lecture on page 17.21
Pump-Probe Geometry Two-Dimensional Spectroscopy
2D-S in the pump-probe geometry is a special case of four-wave mixing,
depicted in Figure 2-8. In this geometry, the third pulse is used as a heterodyne to
observe the third order signal on a detector. Only the third order response which
propagate in the same direction as the third beam are measured. The direction of the
third order signal is determined by equation 2-10, so to make the signal share the
direction of the third pulse, ±�� 1 must equal ∓�� 2. Once again, this does not mean, that
the pulse needs to propagate in opposite directions, only that one pulse interacts with
the ket side and the other with the bra side, or vice versa. The observable signal is a
sum of the system response and its complex conjugate, thus the response shown in
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magenta in Figure 2-8, will also be measured because it is the complex conjugate of the
red response.
Figure 2-8. Illustration of four-wave mixing in the pump-probe geometry and the corresponding third order response signal directions, color coded with the wave vector interactions. Only the qualitative directions are shown.
In DPT, the pump-probe geometry response can be realized if the first two
interactions have opposite directions. For a two-level system, all the cases meet this
condition because two arrows in the same direction and on same bra/ket side are not
possible. But, that is not the case for more complicated systems. The simplest example
where two fields with the same direction is allowed is a three-level system, with states,
A, B, and C. An example is depicted in Figure 2-9.
Figure 2-9. Three level system with two consecutive bra interactions in the same direction represented by DPT.
In the example given in Figure 2-9, the first two interactions have the same
direction, so the third order signal will not be in the direction of the third pulse; the third
order signal will be emitted in the direction of the orange arrow shown in Figure 2-8,
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which corresponds to 𝑘𝑠𝑖𝑔 = −𝑘1 − 𝑘2 + 𝑘3 [a bra side absorption (negative), a bra side
absorption (negative), and a bra side emission (positive)]. The direction of a field is not
the only consideration because �� 𝑖 is a vector and has magnitude; even if the first two
interactions have opposite direction, they will only cancel if they also have the same
magnitude. Interactions like the one depicted in Figure 2-10, would not be measured in
the pump-probe geometry because a field that couples 𝐴 ↔ 𝐵 has a different magnitude
than a field which couples 𝐴 ↔ 𝐶, because |�� | ∝ 𝜔 and 𝜔𝐴𝐵 ≠ 𝜔𝐴𝐶.
Figure 2-10. Four-wave mixing with the first two fields not having the same magnitude
Only signals that co-propagate in the direction as the third pulse are measured in
the pump-probe geometry 2D-S; thus, only signals that go to a population state after the
first two fields are detected. Therefore, 2D-S in the pump-probe geometry yields only
“absorptive signals”. Although pump-probe geometry 2D-S reduces the amount of
information which can be collected in a four-wave mixing experiment, it greatly simplifies
the experiment for two reasons: (1) the pump pulses co-propagate reducing the phase
error associated with thermal phase distortions from different beam paths for optical
frequency pulses, and (2) the weak third order signal co-propagates with the probe
pulse, allowing the probe pulse to heterodyne the signal on the detector and can thus
be measured (see chapter 1 > What is Coherence > Coherent Mixing, to see what is
meant by heterodyne detection). Because the third pulse is used as the heterodyne
reference, the measured 2D-S signal is detected at the same time as the third pulse;
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when the third pulse is not present on the detector, the third order signal is too weak to
measure. Equation 2-8 simplifies to equations 2-11 because 𝑡 = 0; no time is allowed
for the final state to evolve in the pump probe geometry.
𝑅(3) ∝ 𝑒𝑖𝜔𝐵𝐴𝜏 ⋅ 𝑒−Γ𝜏 ⋅ 𝑒−𝑇𝜏𝐵
(2-11)
The 2D-S response in the pump-probe geometry has two independent variables,
𝜏 and 𝑇. The first pulse always put the system into a coherence, so 𝜏 is termed
“coherence time” (“evolution time” in 2D-NMR, but called coherence in pump-probe 2D-
S because it is the time the system evolves in a coherence). In the pump-probe
geometry, the system is always put into a population state by the second pulse, so 𝑇, is
termed “population time” (“storage/mixing time” in 2D-NMR, but called population in
pump-probe geometry 2D-S because 𝑇 represents the time the system spends in a
population state). When 𝑇 is held constant, and 𝜏 is scanned, the result is a signal that
oscillates at the frequency 𝜔 of the transition and decays with Γ as the system losses
coherence. Keeping 𝜏 constant and scanning 𝑇 results in a decaying signal whose
amplitude and sign is determined by 𝜏.
Up to now, the presentation of the simplified theory has not highlighted the utility
of 2D-S. The signals that could be extracted from the presented level of theory could
otherwise be measured by simpler methods: Γ, the decoherence of a state AB can
come from photon-echo experiment looking at how the echo decays as a function of
wait time; 𝜔𝐵𝐴, can be measured by absorption and emission spectra; and the life-time
of the excited state, 𝜏𝐵, can be acquired from a transient absorption experiment. The
potential of 2D-S doesn’t become apparent until the rules of the simplified model are
relaxed, and the system can change states during the evolution time between pulses—a
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more accurate model of what occurs during an experiment. For example, consider the
interaction for three-level system depicted in Figure 2-11.
Figure 2-11. Example of four-wave mixing where the system changes states between two field interactions depicted by DPT.
The first two pulses put the system in the population state |𝐶⟩⟨𝐶|, where it can
evolve during the delay time 𝑇 and even change to state |𝐵⟩⟨𝐵| before the third pulse
arrives. This evolution of the system would result in a 2D-S signal that oscillates with the
frequency, 𝜔𝐴𝐶, detected in state |𝐵⟩⟨𝐵| by the third pulse. By changing the delay time,
𝑇, the transfer from state |𝐶⟩⟨𝐶| to |𝐵⟩⟨𝐵| can be followed in time and the rate
measured. This is the significant advantage of 2D-S over other methods; it allows the
observation of states that are coupled together because a signal will oscillate at the
frequency of the coherence that it originates from.
The potential to measure the coupling between states allows many processes to
be measured. For example, 2D-S can measure inhomogeneous broadening of a line
shape because the signal oscillates at the natural frequency, even though it would be
measured in all the possible micro environments probed at different delay times, 𝑇.
2D-S can also measure coherent and incoherent coupling of states. A coherent
superposition of states results in the 2D-S signal where the population of two states
oscillate between the two states as 𝑇 is scanned. An incoherent coupling of states is
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measured as the decay of one population, and growth of another as the population of
one state is transferred to the other state without an oscillating behavior.
Having introduced the theory, the focus will shift on matching theory with
experimental implementation.
Experimental Introduction
Figure 2-12. Simplified diagram of a pump-probe geometry experimental setup.
All the components needed for a pump-probe geometry 2D-S experiment are
diagramed in Figure 2-12. A pulsed ultrafast laser is used to produce a fundamental
coherent pulse, from which all other pulses will originate. It is important to use the same
laser to generate all the pulses used for an experiment, because 2D-S is only sensitive
to phase differences; if all the pulses experience the same phase change because of
laser phase drift, it will not affect the data. The fundamental laser we use is a
commercial chirped-pulse amplified laser, SpitFire (Spectra-Physics) operating at a
repetition rate of 1 kHz with 800 nm central wavelength. The fundamental gets split into
< 1 𝑝𝐽
~2 𝜇𝐽
Δ𝑡 ~ 400 fs
Δ𝜆 ~ 100 nm
~ 100 𝜇𝐽 Δ𝑡 ~ 50 fs Δ𝜆 ~ 25 nm
~100 𝑛𝐽 Δ𝑡 ~ 28 fs Δ𝜆 ~ 100 nm
𝝉 : 0 - 1.4 ps 𝝉
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two parts, with most laser energy/pulse going to generate the first two pulses in 2D-S.
We call these pulses “pumps” because of the pump-probe geometry. Generally, the
system of interest is at a different wavelength than the fundamental laser, so some
wave mixing method is used to change the wavelength of the fundamental to a different
range. A fraction of the split fundamental not used to generate the pump pulses is used
to generate the third pulse, which we refer to as the “probe”. After generating the
desired pump pulse wavelengths, the pump pulse is taken to a pulse shaper, which can
modulate the pump pulse to generating a pulse pairs with a controllable time spacing 𝜏.
The pumps and probe are overlapped(superimposed) on a sample in space and time, to
generate the 2D-S signal. The probe, which co-propagates with the 2D-S signal is then
frequency resolved and measured using a spectrograph and CCD camera. The signal is
digitized and sent to a computer for signal analysis.
The breakdown of the individual components will be explored further, part by
part. The following is required for a 2D-S experiment in the pump-probe geometry:
Two pump pulses with-
• Spectral bandwidth covering the absorption range of interest
• Enough pulse energy to excite a detectible signal (system dependent: pJ-mJ)
• Pulse width shorter than the dynamics to be studied
• Stable and controllable phase
• controllable delay 𝜏 One probe pulse with-
• Spectral bandwidth covering as much range as possible
• Pulse width shorter than the dynamics to be studied
• Detectible intensity for the heterodyne cross term signal
• Fixed and controllable delay 𝑇 between pump and probe
Broadband detector with-
• Ability to spectrally resolve signal
• High sensitivity to distinguish weak oscillations from noise
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Two Pump Pulses
2D-S requires three pulses to generate the third-order signal. The first two pulses
are called pump pulses because they initiate the coherence and then put the system
into a population state. The fluence of a field is linearly dependent to the probability of a
transition, in the weak-field limit. Thus 2D-S signal is dependent to pump fluence; you
want the most fluence while maintaining linear absorption.
The spectral bandwidth of the pump pulses is important because only transitions
with frequencies within the pump bandwidth will yield 2D-S signal. To measure the
coupling between two states, the pump bandwidth must contain both transition
frequencies; the major difference between 2D-NMR and optical 2D-S. For example, all
of 2D-NMR can be collected with less frequency bandwidth (bandwidth 0 to ~1 GHz),
than observing a red (650 nm, 461 THz) and orange (590 nm, 508 THz) transition,
which would require 47,000 GHz of bandwidth. Given the technical constraints of
generating pulses with enough bandwidth and fluence, systems studied by optical 2D-S
are limited to where in the UV-VIS spectrum pulses can be generated.
In the last 20 years, a new versatile method has been developed that allows the
generation of very broadband optical pulses, with enough energy and phase stability
between the different frequencies components. The method is based on optical
parametric amplification (OPA) of non-collinear propagating pulses. Coined NOPA,
because of the noncolinear propagation between the pump and seed, compared to
traditional OPAs.
Noncollinear optical parametric amplifier
A NOPA is based on a tunable inflection point in the phase matching condition
for a Type I non-linear crystal which is multi angle dependent22, depicted in Figure 2-13.
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Figure 2-13. Depiction of angles involved in NOPA phase matching. A) Diagram of important angles, B) change in phase matching conditions as a function of pump and signal angles. Figures reprinted from Optics Communications, Vol. 203, P. Tzankov,
I. Buchvarov, T. Fiebig, Broadband Optical Parametric Amplification in the Near UV-VIS, pp. 107-113, copyright (2002), with permission from Elsevier.
By controlling the cut of the crystal, and the angles of the incoming beams, the
phase matching region of crystal can be made much broader than if the signal and
pump traveled colinearly. The effect of the angle of the crystal on the bandwidth
generated is illustrated in Figure 2-14.
Figure 2-14. NOPA spectrum dependence as a function of phase matching angle in BBO. Figures reprinted from Optics Communications, Vol. 203, P. Tzankov, I. Buchvarov, T. Fiebig,
Broadband Optical Parametric Amplification in the Near UV-VIS, pp. 107-113, copyright (2002), with permission from Elsevier.
NOPA/OPA theory is based on non-linear 3-wave mixing interaction, where a
pump pulse interacts with a seed pulse, transferring energy to generate a signal pulse,
and an idler pulse. The theory is more complicated than 2D-S theory because it is a
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non-linear 3-wave mixing process, so I will not go into detail. Theory, math, and
parameters to make a NOPA are covered very clearly in work by Fiebig.22 The gist of
NOPA/OPA theory: waves will only coherently interact (needed for non-linear
interactions), if they remain phase locked relative to each other. All materials have a
wavelength/frequency dependent dispersion, so two distinct colors will travel at different
speeds inside a medium because they each experience a different dispersion, causing
a phase drift. Phase drift results in decoherence, preventing coherent mixing.
Birefringent crystals have two independent dispersion axes, called ordinary and
extraordinary. Two beams of distinct color can co-propagate in a non-linear crystal if a
condition exist where one beam experiences the dispersion of the ordinary axis and the
other the dispersion of the extraordinary axis, and the dispersions are equal. This
condition is called, “phase-matching” because both beams experience the same
effective dispersion, and thus will not de-phase, allowing coherent non-linear mixing.
The angle of the crystal needed to achieve phase matching is called the phase
matching angle. The spectral bandwidth range (color range) that can phase match in a
non-linear crystal, determines the range which can be amplified by coherent mixing.
Adding an angle between the two mixing beams allows for more bandwidth phase
matching at the inflection points of some phase matching angles, shown in Figure 2-14.
The NOPA we built was based on the design by the Miller group which takes
advantage of anamorphic focusing to enhance the bandwidth generation.23 Through
anamorphic focusing of the 400 nm pump beam on the NOPA BBO, there can be two
different perpendicular focus lengths for the pump beam. The axis which corresponds to
the extraordinary dispersion axis of the crystal can have a tight focus because this is the
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direction which determines phase matching. The axis of the pump not involved with
phase matching can have a longer focus, allowing for more pump energy in the
bandwidth generation axis with a reduced risk of damaging the BBO. Figure 2-15
compares the increased bandwidth obtained through anamorphic focusing with a
spherical focusing NOPA of similar pump energy.
Figure 2-15. Comparison of NOPA spectrum generated with anamorphic focusing and spherical focusing. Figure reproduced from Johnson, P. J.; Prokhorenko, V. I.; Miller, R. J.
Enhanced bandwidth noncollinear optical parametric amplification with a narrowband anamorphic pump Opt. Lett. 2011, 36, 2170-2172.
A schematic of the NOPA we build is found in Figure 2-27. We made
modifications compared to the Miller group design23: we used a dichroic mirror as a
harmonic separator (splitting 800nm/400nm) to use the leftover fundamental 800 nm
from second harmonic generation to create white light for the seed of the NOPA. We
also moved the delay line from the seed beam to the pump beam because of space
constraints. The cut for the NOPA BBO and the external angle are different from the
original design because our fundamental laser is at a different wavelength than the
Miller group; our NOPA BBO crystal is cut at 31.55 degrees, with no coating. The high
fluence of the 400 nm pump would burn any AR or protective coating. The external
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angle between the pump and white light seed is 2.8 degrees, with the seed beam
normal to the crystal face. The equations needed to determine the cut of the crystal and
external angle are shown by Fiebig22. A list of important optics in the NOPA we built
can be found in Table 2-1. The spectrum of our NOPA is shown in Figure 2-16.
Figure 2-16. Optimized spectrum of the NOPA with an output energy of 2.0 𝜇J/pulse.
Pulse shaping
A commercial pulse shaper, SLM-640 (CRI, Cambridge MA), was used to
achieve the last requirements needed for the two pump pulses: Short duration, fixed
and controllable phase, and controllable delay between pump pulses.
The dual mask SLM-640 is a light modulator that can alter the phase and
amplitude of a horizontally polarized incident laser pulse using birefringent liquid
crystals. The SLM works by independently controlling 640 pixels per LCD mask through
an applied voltage. When a voltage is applied to each independent pixel, crystal in each
pixel align with the field increasing their extraordinary index of refraction. The SLM takes
advantage of the change in extraordinary index of refraction to change the amplitude
and/or phase of the laser pulse, behaving as a wave retarder. A simplified illustration of
how an SLM works is shown in Figure 2-17.
0
Wavelength (nm)
Inte
nsity
(ar
b.)
450 500 550 600 650 700
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Figure 2-17. Illustration of how individually controlling SLM pixels for a pulse in the Fourier plane can alter the phase and amplitude. This figure does not capture the true mechanism of the SLM, because both makes change the phase and amplitude simultaneously. Part A is adapted from Nuernberger, P.; Vogt, G.; Brixner, T.;
Gerber, G. Femtosecond quantum control of molecular dynamics in the condensed phase Phys. Chem. Chem. Phys. 2007, 9, 2470-2497. Part B was produced by Valeria D. Kleiman and reproduced with permission.
Pulse shapers modulate the pulse in the Fourier plane, where each induvial
frequency is separated in space. A 4-f compressor is needed to take the pump pulse
into the Fourier plane, and then recombine the pulse after it has been modulated. A
simplified illustration of a 4-F compressor is shown in Figure 2-17A. The 4-f compressor
design we used came from a former group member who went through the work of
determining the best 4-f configuration to reduce distortions on the beam.10 The 4-f
designed was for 800 nm pulses, making it impractical to make simple changes to adapt
for visible light. We kept the location of the major optical components, but instead of
using polarization to extract the incoming and outgoing beam (A faraday rotator which
would work for the entire NOPA bandwidth was not available), we used a small angle in
the beam path to spatially separated the beams. The spatial separation allows for a
pick-off mirror to be used. The design of the tilted 4-f compressor is shown in Figure 2-
18. The design we used is called a tilted folded 4-f compressor and is described in more
detail in Chapter 3.
A B
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Figure 2-18. Tilted folded 4-f compressor diagram.
One Probe Pulse
For 2D-S in the pump probe geometry, the probe pulse works as both the third
pulse and a heterodyne local oscillator for the third-order signal. The range of
wavelengths that can be probed is limited to the bandwidth of the third pulse (excluding
detector and optics limitations), thus the use of broadband continuum (white light). In
addition, the temporal resolution of the experiment is affected by the pulse width.
Generating a broadband continuum is achieved by tightly focusing an ultrafast laser
pulse on clear medium such as sapphire or bulk glass, resulting in self phase
modulation from the high intensity yielding a broadband laser pulse which is also short
in time.24 The spectrum of the supercontinuum is dependent on the fluence of the tightly
focusing pulse, a typical spectrum generated in sapphire with an 800 nm pulse is shown
in figure 2-19.
The probe pulse needs to be low intensity for two reasons: (1) a sensitive
detector is needed to distinguish noise oscillations from 2D-S signal, and sensitive
detectors saturate easily; (2) the intensity of the probe needs to be low enough to not
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overshadow the intensity of the heterodyne term. A white light continuum generated in
sapphire has energy in the pico-Joules, already close to the saturating limit of CCD
cameras.
Figure 2-19. Typical white light spectrum generated in sapphire with different fluence. The intensity is not normalized.
Accurate and precise delays of the third pulse are also needed to maintain
control of the population time 𝑇. Phase stability is not critical for the third pulse
(population states are invariant to phase) so a commercial optical delay line can be
used. We use a ThorLabs DDS220 (New Jersey) which has a 220 mm range with
reproducibility down to ±0.5 fs, in a single pass retroreflector configuration.
Broadband Detector
2D-S signal is weak because it is a third-order signal originating from three weak
perturbations. Going back to equation 1-11, to measure the cross term (heterodyne) to
extract the 2D-S signal, the amplitude squared of the probe pulse cannot be significantly
greater than the amplitude of the probe pulse multiplied with the amplitude of the 2D-S
signals. The limit to which 𝐴𝑝𝑟𝑜𝑏𝑒2 can be distinguished from 𝐴𝑝𝑟𝑜𝑏𝑒 ⋅ 𝐴2𝐷−𝑆 is detector
dependent. CCDs are ideal to look for the oscillations of 𝐴𝑝𝑟𝑜𝑏𝑒 ⋅ 𝐴2𝐷−𝑆 as 𝜏 is scanned
because they are multi-element detectors with high sensitivity and low noise. Coupling a
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CCD to a spectrograph allows the individual pixels of the CCD to spectrally resolve the
2D-S signal. In our experiments, we combine a 260i spectrograph (Oriel, Oregon) and a
MicroMax CCD camera (Roper Scientific, New Jersey) to collect the 2D-S signal. The
configuration of the spectrograph with the size of the CCD chip, allows us to collect a
range of wavelengths from 430 nm to 655 nm when a 150 𝑔𝑟
𝑚𝑚 grating is used. This
range is tunable because the grating is rotatable, changing the central wavelength. The
spectrograph has 3 different gratings (1200 𝑔𝑟
𝑚𝑚, 600
𝑔𝑟
𝑚𝑚, and 150
𝑔𝑟
𝑚𝑚) giving us the
ability to change the dispersion on the CCD to look at smaller range of wavelengths with
better spectral resolution.
Making Raw Data Meaningful
Now that the theory and method has been introduced, the focus shifts to turning
measured data into something meaningful and “easy” to interpret. Like 2D-NMR, the
raw time-domain data contains lots of information, but in a format not easy to interpret.
Through signal processing (Fourier Transformation), the time-domain data are
converted to a frequency-domain spectrum. Figure 2-20 shows a caricature often used
to explain how to read a 2D-S plot. A three-level system is used with two transitions
from the ground state at frequency, 𝜔𝐴𝐶 and 𝜔𝐴𝐵. Other transitions will be ignored for
the simplified explanation (i.e. no stimulated emission). 2D-S data is a 3D matrix
because there are 3 parameters, 𝜔𝑒𝑥𝑐𝑖𝑡𝑎𝑡𝑖𝑜𝑛 (FFT of 𝜏), 𝜔𝑑𝑒𝑡𝑒𝑐𝑡𝑖𝑜𝑛, and 𝑇. There is no
way to represent a 3D matrix as a figure on a two-dimensional sheet of paper, so only
slices at constant T are plotted, either alone or as series adjacent to each other to
represent 𝑇 time evolution. In dynamic two-dimensional media (i.e. movie) the 𝑇 slices
can be shown as snapshots in a film. Figure 2-20 shows a single T slice of “data” for a
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3-level system. The dashed line is called the diagonal because it represents signals
excited and detected at the same frequency (𝜔𝑒𝑥𝑐𝑖𝑡𝑎𝑡𝑖𝑜𝑛 = 𝜔𝑑𝑒𝑡𝑒𝑐𝑡𝑖𝑜𝑛). If population from
state C decays into state B, a signal will be detected at 𝜔𝑑𝑒𝑐𝑡𝑖𝑜𝑛 = 𝜔𝐴𝐵 when
𝜔𝑒𝑥𝑐𝑖𝑡𝑎𝑡𝑖𝑜𝑛 = 𝜔𝐴𝐶, referred to as an off-diagonal peak because signal is detected at a
different frequency than the excitation (implying coupling between the two states in this
example).
Figure 2-20. Simplified caricature of 2D-S data to explain on-diagonal and off-diagonal signals.
Optical 2D-S Pump-Probe Spectroscopy is a Differential Spectroscopy
Unlike 2D-NMR, a 𝜋-pulse to prepare a pure population state (other than the
ground state) is not possible in optical spectroscopy. Instead optical two-dimensional
spectroscopy operates in the weak field limit were only a fraction of the population is
transferred to an excited state (the linear range of Rabi-oscillation). Thus, optical 2D-S
is a differential spectroscopy, comparing the change in unperturbed ground state
absorption, with an absorption with a fraction of population in the excited state. The
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caricature shown in Figure 2-20 does not represent what an optical 2D-S signal will
measure because a differential optical spectrum is cluttered with many overlapping
signals at the same detection frequency. Extracting useful information from an optical
2D-S experiment is quite challenging and still an unsolved problem in the relativly new
field of optical frequency 2D-S. In Chapter 4, I will show how I extracted information
from a 2D-S experiment by coupling what was learned from TA experiments (a slice of
2D-S data in the pump-probe geometry corresponds to an equivalent TA experiment at
the corresponding excitation wavelength, covered next).
A Slice of Pump-Probe 2D-S Data Corresponds to a TA experiment
As an example, 2D-S data I collected for the laser dye DASPI will be presented
to explain 2D-S signals, comparing to published transient absorption (TA) data of
DASPI25 for validation. I am the first person (besides the Miller group) to successfully
build and use the blue-green NOPA for any experiment. Giving a hint to the complexity
of the instrument; many other ultrafast groups tried to use the blue-green NOPA for
experiments because of the many interesting and unstudied systems accessible only by
the NOPA designed by the Miller group. The Miller group only published one article26
(conference paper) using the anamorphic NOPA for 2D-S experiments preformed in the
box-car geometry using diffractive optics. I am the first to collect pump-probe geometry
2D-S data using the blue-green NOPA (hence the need for an extensive Chapter 3
covering all the problems we needed to overcome). There is no choice but to use a well-
studied molecule (DASPI) to benchmark our instrument because no published pump-
probe 2D-S exists to reproduce in the wavelength range our instruments operates in.
DASPI 2D-S data was collected in methanol, at room temperature, in a 2 mm optical
path cuvette with an optical density of 0.3 OD at 480 nm. The sample was stirred with a
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PTFE coated magnetic stir bar to avoid heating effects from the laser. The pump pulse
energy was ~15 nJ/pulse with a spot size of ~170 𝜇m. The probe pulse was a
broadband continuum, generated in sapphire, with a spot size of ~80 𝜇m at the sample
position.
Figure 2-21. Raw 2D-S data for DASPI scanning 𝜏 at constant 𝑇 = 30 𝑓𝑠. A) Data for all detection wavelengths seen by CCD, B) a single detection wavelength, the colored dots relate to Figure 2-22
Figure 2-21A is a plot of the signal measured by the CCD at a fixed 𝑇, while
scanning 𝜏 for DAPSI. This signal is given by the change in intensity of the probe
(Δ𝐶𝑜𝑢𝑛𝑡𝑠) as a function of detection wavelength and delay 𝜏 between the two pumps.
A
B
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Figure 2-21B shows a single detection wavelength (one horizontal slice of Figure 2-
21A). The 2D-S signal is governed by equations 2-11, when 𝑇 is held constant, the
signal will oscillate with a decay. Figure 2-22 shows the 2D-S signal when 𝜏 is held
constant, and 𝑇 is scanned. The signal will appear as a TA trace with signal sign and
amplitude governed by 𝜏.
Figure 2-22. Raw 2D-S data for DASPI scanning 𝑇 and constant 𝜏. Line colors correspond to equivalent color coded 𝜏 in Figure 2-21B
Data presented in Figures 2-21 and 2-22 in the time-domain are not easy to
interpret and extract information. A Fourier transform along the 𝜏 dimension is
preformed to convert to 𝜔𝑒𝑥𝑐𝑖𝑡𝑎𝑡𝑖𝑜𝑛. UV-Vis spectroscopy is typically reported in
wavelength, so 2D-S plots have 𝜆𝑒𝑥𝑐𝑖𝑡𝑎𝑡𝑖𝑜𝑛 instead. Figure 2-23A shows processed data
for the raw data shown in Figure 2-21, represented in Δ𝑇𝑟𝑎𝑛𝑠𝑚𝑖𝑠𝑠𝑖𝑜𝑛. Figure 2-23B
shows data for a different 𝑇 time at 750 fs, after the dye DASPI has red shifted
(explained when TA data is introduced). The units for plotting 2D-S data are not yet
established in the community, some use Δ𝑇𝑟𝑎𝑛𝑠𝑚𝑖𝑠𝑠𝑖𝑜𝑛, and others use Δ𝐴𝑏𝑠𝑜𝑟𝑝𝑡𝑖𝑜𝑛.
We choose Δ𝐴, because it shows data in a log scale, thus making weaker signals more
noticeable. Figure 2-24 shows DASPI data in Δ𝐴. Keeping track of the absolute intensity
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of a signal is difficult after an FFT, so 2D plots are often in relative units, either
normalized, or just keeping the intensity output of the FFT.
Figure 2-23. Processed 2D-S data for DASPI at two different 𝑇 values shown in Δ𝑇𝑟𝑎𝑛𝑠𝑚𝑖𝑠𝑠𝑖𝑜𝑛. A) 𝑇 at 100 fs, B) 𝑇 at 750 fs
Figure 2-24. Processed 2D-S data for DASPI at two different 𝑇 values shown in Δ𝐴𝑏𝑠𝑜𝑟𝑝𝑡𝑖𝑜𝑛. A) 𝑇 at 100 fs, B) 𝑇 at 750 fs.
The processed 2D-S plots shown in Figure 2-23 and 2-24 are still too
complicated for anyone other than an expert in optical 2D-S to extract information.
A B
A B
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Figure 2-25. Published TA DASPI data. Figure explained in text. Reprinted from Bingemann, D.;
Ernsting, N. P. Femtosecond solvation dynamics determining the band shape of stimulated emission from a polar styryl dye J. Chem. Phys. 1995, 102, 2691, with the permission of AIP Publishing.
To help explain what the data represents, published TA results for DASPI in
methanol excited at 470 nm will be introduced. Figure 2-25 shows the information
needed from a steady-state measurement and TA experiments needed to help interpret
2D-S data. Figure 2-25A shows the absorption and emission spectrum of DASPI in
methanol. Figure 2-25B shows the composition of the TA signal where ESA is excited
A
B
C
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state absorption (a positive signal), ABS is ground state bleach (a negative signal
associated with missing ground state absorption), and GAIN is stimulated emission (a
negative signal that shifts in time as the excited state cools from a hot vibrational state,
until finally settling at the ground vibrational state of the excited electronic state). Figure
2-25C shows snap shots of the TA spectrum collected at different probe delays.
Figure 2-26 plots 2D-S data next to TA data, with slices of the 2D-S plot which
correspond to a TA experiment; pump-probe 2D-S experiment is an excitation
wavelength resolved TA experiment.
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Figure 2-26. A slice of pump-probe 2D-S data for a given excitation wavelength correspond to an equivalent TA experiment at the same excitation wavelength. A) 2D-S data collected for DASPI at 𝑇 = 750 𝑓𝑠 with the white dashed line representing the diagonal, B) Slice of 2D-S plot at 477 nm excitation, C) published TA data for DASPI collected at 470 nm excitation with ~60 fs pulses, lines are color coded with part B. Part C of this figure was adapted from
Bingemann, D.; Ernsting, N. P. Femtosecond solvation dynamics determining the band shape of stimulated emission from a polar styryl dye J. Chem. Phys. 1995, 102, 2691, with the permission of AIP
Publishing.
𝑻 = 𝟕𝟓𝟎 𝒇𝒔
𝑇 (𝑓𝑠) 200 300 750
A
B
C
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Table 2-1. List of optics used in the NOPA with numbers associated with Figure 2-23.
Optic Number
Optic Type Description Company
1 SHG-BBO 1 mm BBO cut for 800 nm SHG. AR coated (800 nm Front / 400 nm Back)
New light photonics
2 Dichroic Mirror Transmits 400 nm and reflects 800 nm. 99.9% R of 800 nm and 98% T of 400 nm.
CVI
3 Retroreflector Hollow-corner cube reflector. Protected aluminum
Melles-Griot
4 Cylindrical Lens 25.4 mm square cylindrical singlet lens focusing vertically. +750 mm focus at 633 nm
CVI
5 Cylindrical lens 25.4 mm square cylindrical singlet lens focusing horizontally. +250 mm focus at 633 nm
CVI
6 NOPA BBO 1 mm BBO cut at 31.55º. No coating United Crystals
7 Variable ND Filter Reflective variable ND filter 0.01-4.00 OD ThorLabs
8 Spherical Lens 25.4 mm round singlet lens, AR coated for 800 nm. +50 mm focus at 633 nm.
CVI
9 Sapphire Window High quality 2 mm thick, 1 inch window with no coating.
CVI
10 Off-axis Parabolic Mirror
50.8 mm optic with 25.4 mm effective focal length. Protected aluminum.
Newport
11 Spherical Mirror 25.4 mm round concave mirror with protected silver coating. +500 mm focus.
CVI
12 Spherical Mirror 50.8 mm round concave mirror with protected silver coating. +250 mm focus.
CVI
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Figure 2-27. NOPA schematic. A list of optics corresponding to the numbers next to optics is provided in Table 2-1. Black
lines represent mirrors. The linear polarization states of the beams are: 800 nm is vertical, 400 nm is horizontal, white light seed is unpolarized, NOPA generation is vertical, and the final polarization leaving the NOPA horizontal. The turning mirror, circled in yellow, of the 400 nm path, determines the angle between the pump and probe, and is used for pump-probe overlap at the NOPA BBO.
12
3
4
5
6
8
9
7
10
11
12
Turning periscope
𝛼𝑒𝑥𝑡 = 2.8°
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CHAPTER 3 IMPLEMENTATION AND TROUBLESHOOTING
“Lasers bring more misery than happiness; but, more lasers more fun.” Nico Omenetto
Having introduced 2D-S basics in Chapter 2, focus will now shift to much more
technical information required to build, preform, and analyze a pump-probe 2D-S
experiment and avoid the many pitfalls we faced because 2D-S is not yet a turn-key
method. This chapter will assume an advanced understanding of spectroscopic
methods and theory that have not been introduced. Several books10,13,27-29 are
recommended to help the reader follow this chapter.
Figure 3-1. Simplified diagram of a pump-probe geometry experimental setup.
Each instrument and their problems will be introduced in the order that the laser
beam propagates, starting where the fundamental laser beam is split for the NOPA
generation and ending at the CCD. Then focus will shift to data collection and analysis,
< 1 𝑝𝐽
~2 𝜇𝐽
Δ𝑡 ~ 400 fs
Δ𝜆 ~ 100 nm
~ 100 𝜇𝐽 Δ𝑡 ~ 50 fs Δ𝜆 ~ 25 nm
~100 𝑛𝐽 Δ𝑡 ~ 28 fs Δ𝜆 ~ 100 nm
𝝉 : 0 - 1.4 ps 𝝉
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including the important things we learned that should be passed on. The layout of the
instrument is shown in Figure 3-1.
NOPA Generation
Figure 3-2. Some typical NOPA spectrum achievable day-to-day with energies between 1.5 to 1.8 𝜇J/pulse.
The NOPA we built was designed around anamorphic focusing to enhance
bandwidth generation23, introduced in Chapter 2. A schematic of our NOPA can be
found in Figure 2-27. The intensity spectrum generated by a NOPA is very sensitive to
the external angle of the pump/seed beams and spatial-temporal overlap, making it
difficult to reproduce the optimized spectrum and energy per pulse shown in figure 2-15.
The seed used for the NOPA will be discussed later. Many hours of labor are needed to
optimize the NOPA generation to be “optimal”, 2 𝜇J/pulse with full bandwidth. Day-to-
day laser fluctuations require the NOPA to be constantly realigned. Instead of focusing
our time and energy on getting the optimal NOPA generation, we optimize until a
“workable” NOPA spectrum for an experiment is generated (we are not energy limited in
our 2D-S experiments so getting the most power is not important). The intensity spectra
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shown in Figure 3-2 are typical NOPA spectrums that can be achieved daily with only
30-60 min of optimization by an experienced user. Workable spectrums for an
experiment needs to cover the full range of wavelengths that are modulated by the
pulse shaper (475 nm to 565 nm, explained later).
NOPA generation of at least 1.45 𝜇J/pulse is recommended to ensure that the
spectrum will remain stable throughout an experiment (~20-30 hours). The stability of a
NOPA is energy dependent, too little power and it is unstable, too much power and it is
also unstable (1.5 to 2.0 𝜇J/pulse is the “sweet-spot” of our system). The NOPA cannot
be pumped with more energy than the designed 12 𝜇J/pulse of 400 nm at the crystal
position, because the design is near the damage threshold for an uncoated 𝛽 −barrium
borate (BBO) crystal.
A known issue of anamorphic focused NOPA design is the resultant spatial chirp
(wavelengths spread in space) from anamorphic focusing seen in Figure 3-3A.
Figure 3-3B shows that tightly focusing the pump in the phase matching direction
results in a sweep of angles of the pump inside the BBO crystal given by 𝛿𝛼𝑖𝑛. The
different angles inside the crystal, edges shown in red and green lines, will experience
different phase matching angles, a sweep from red to green angle in Figure 3-3B.
Figure 3-3C shows the phase matching conditions dependence on the phase matching
angle, NOPA spectrum generation at the edges will not be equal. The smaller angle
(green) generates more of the inner wavelengths and the large angle (red) the outer
wavelengths.
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Figure 3-3. Spatial chirp from anamorphic focusing NOPA generation is the result of a large sweep of phase matching angles inside the crystal. A) Collimated NOPA beam immediately after generation imaged on a diffuser, B) illustration of different phase matching angles inside the crystal, C) different phase matching angles will give different phase matching conditions inside the crystal. Figures adapted from Johnson, P. J.; Prokhorenko, V. I.; Miller, R. J. Enhanced bandwidth
noncollinear optical parametric amplification with a narrowband anamorphic pump Opt. Lett. 2011, 36, 2170-2172.
A
C
B
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The beam profile shown in figure 3-3A shows the spatial chirp (horizontal)
immediately after generation. The NOPA generation is vertically polarized from type I
phase matching conditions in the NOPA BBO crystal. Our pulse shaper requires
horizontally polarized light (determined by AR coatings on the SLM arrays). To change
the polarization of our beam to meet our needs, a turning periscope immediately after
NOPA generation is used. Turning the beams polarization with a turning periscope also
turns the spatial chirp on its side (spatial chirp will now be in the vertical direction).
The spatial chirp of our NOPA beam was measured by imaging the beam after
first order diffraction onto a CCD. Figure 3-4A shows the spatial chip with wavelengths
resolved in the x-axis, and physical space in the y-axis. The spectral chirp we observe
matches the expectations from the different phase matching conditions, shown in Figure
3-3C. We compensate the negative spatial chirp of the NOPA beam (crescent shape),
by introducing opposite spatial chirp (upside down crescent shape) with the geometry of
the 4-f compressor (explained later). Figure 3-4B shows the spatial chirp of the NOPA
beam after the 4-f compressor.
Figure 3-4. Spatial chirp of NOPA beam measured by imaging first order diffraction on a CCD. A) Collimated NOPA after the turning periscope, before the 4-f compressor, B) collimated NOPA after travel through our tilted 4-f compressor. The wavelength difference is a result of day-to-day NOPA spectrum changes, not from the 4-f compressor.
A
B
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Pulse Shaping
There are two major components involved with pulse shaping: (1) diffracting the
beam into wavelength components and collimating into the Fourier plane using a 4-f
compressor, and (2) applying a modulation mask, by changing the phase and
amplitudes of individual wavelengths with a spatial light modulator. Figure 3-5 shows a
simplified illustration of pulse shaping.
Figure 3-5. Simplified illustration of pulse shaping. A) the beam is diffracted into wavelength components using a grating then collimated into the Fourier plane. B) The pulse can me modulated by changing individual wavelength phase and amplitude. This figure is not accurate representation and only an illustration to simplify understanding. Part A is adapted from Nuernberger, P.; Vogt, G.;
Brixner, T.; Gerber, G. Femtosecond quantum control of molecular dynamics in the condensed phase Phys. Chem. Chem. Phys. 2007, 9, 2470-2497.. Part B was produced by Valeria D. Kleiman and reproduced with permission.
Tilted 4-f Compressor
A 4-f compressor uses a diffraction grating to disperse wavelength components
of a beam in space. The dispersed beam is then collimated with a focusing optic,
effectively taking a pulse from the time domain to the frequency domain (called the
Fourier plane because wavelengths are separated in space and the phase of each
wavelength determines the pulse in the time domain). The SLM-640 we use is a double
pass configuration (there is a mirror at the end to reverse propagate the beam back
through the SLM). Travelling through the SLM twice doubles the dynamic range of the
SLM by doubling the effect of each pixel array, but it requires a folded 4-f compressor
A B
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design which can distinguish the beam entering the shaper from the beam exiting the
shaper. An innovative design by Kuroda30, uses polarization changes to distinguish
between incoming and outgoing beams to minimize spatial chirp and pulse front tilt. The
design does not work for us because the design is for 800 nm pulses, and our spectrum
is in the blue-green of the visible, where optics for bandwidths of ~100 nm don’t exist for
polarization separation.
Figure 3-6. Tilted folded 4-f compressor design. Optics described in text.
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Being unable to use polarization led us to go back to the standard method for
extracting pulses from a folded 4-f compressor, using tilt in the beam propagation (see
Figure 3-6). A small angle between the incoming and outgoing beam will lead to spatial
separation after a long path, allowing a pick-off mirror to separate the beams. A known
issue of a tilted 4-f compressor is resulting spatial chirp, because the incoming and
outgoing beam cannot share the true focal point of the focusing optic. The resulting
spatial chirp is crescent shaped because of focal point mismatch. By choosing whether
the incoming or outgoing beam matches the focal point of the focusing optic the beam
can have spatial chirp crescent concave up (incoming matches focus) or concave down
(outgoing matches focus). The spatial chirp of the NOPA beam entering the shaper is
concave down (see Figure 3-4A) choosing the incoming beam to match the focus of the
optics effectively cancels spatial chirp (see Figure 3-4B). The tilt angle was determined
experimentally. Our tilted 4-f design, depicted in Figure 3-6, has an incoming and
outgoing beam separated by ~6 mm after 250.4 cm of travel (distance to and from pick-
off mirror). The grating has grove density 1800 𝑔𝑟
𝑚𝑚, with a protected aluminum coating,
nominal blaze of 21.1°, and ~80% -1 order reflectivity for 400-600 nm horizontally
polarized light (Richardson Grating, catalog number 53-*-289R). The focusing mirror is
a 15.24 cm round concave protected aluminum mirror, with a focal length of 30.48 cm
(Edmunds optics, catalog number 32-839). The polarizer is a thin sheet polarizer with
an extinction ratio of 6000:1 dB (Newport, catalog number 5511). A calcite polarizer
cannot be used, because the NOPA pulse generates white light in the calcite. All other
optics are flat protected silver mirrors. The optics chosen for the 4-f compressor are
determined by SLM, discussed further below.
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Using a concave spherical mirror is not ideal in a 4-f compressor because it
focuses the beam vertically as well as collimating the colors horizontally. The unneeded
focus in the vertical direction makes the distance from the SLM to the focusing mirror
critical, if the SLM back mirror is not at the exact focus of the focusing mirror, the beam
leaving the 4-f compressor will not be collimated. We have no choice but the use a
spherical mirror in our design because the SLM-640 pixel arrays are deformed30, not
focusing the beam onto the SLM face would result in serious spatial chirp (shown in
Figure 3-7). Focusing onto the SLM array minimizes spectral distortion on the beam
(like how a person with astigmatism can see sharper images by squinting, minimizing
the d).
The wavelength dispersion of the 4-f compressor on the SLM-640 is important
because the system is pixelated and a continuous phase function in wavelength is not
possible, leading to pixilation issues in modulation masks. The optimal 4-f configuration
and wavelength dispersion in the Fourier plane for an SLM-640, has been previously
calculated30, an 1800 𝑔𝑟
𝑚𝑚 grating is needed to disperse the beam with a focusing mirror
of focal length ~30.48 cm to collimate the beam into the Fourier. Pixilation effects in a
phase mask are covered in detail by Kuroda30 and Damrauer31. The most important
result from pixilation is that there is maximum phase difference between two adjacent
pixels of 2𝜋, limiting the dynamic range a pulse can be moved in time. For a pulse
centered at 520 nm (NOPA spectrum center) with the above grating-focus optic combo,
the dynamic range is ~2 ps.
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Figure 3-7. Spatial aberrations introduced by the SLM-640 when a cylindrical mirror is used. Each panel shows the spatial distortions at different SLM-640 positions in the focal plane of the 4-f compressor. A) Center of SLM array at ~ 500 nm in the Fourier plane, B) ~520 nm C) and ~540 nm.
Figure 3-8 shows the spectral bandwidth allowed through the SLM by a 4-f
compressor with the grating-focal combo described above is shown in orange. The
dash-black lines show where the beam gets cut off by the edges of the SLM array. Only
intensity in the spectral range allowed through the SLM is relevant for an experiment, all
other wavelengths get blocked. Therefore, it is not important to maximize the bandwidth
of the NOPA generation, only ensure that the spectrum covers the full range of the
SLM. The blue spectrum is the NOPA spectral bandwidth before the shaper to compare
with the spectrum after the shaper.
Figure 3-8. Spectral bandwidth of the pump pulse allowed through the SLM-640 array, with the 4-f compressor design used. Black lines show the edges of the pixel arrays, were spectrum hits the edges of the SLM-640 device. Blue is spectrum before the shaper, and orange is the spectrum after the shaper. The difference in intensity distribution is a result of optic efficiency not being equal at all spectral wavelengths.
B C A u
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The efficiency of the 4-f compressor, including the SLM, is measured at ~11%
(energy in over energy out). The difference in intensity profile between pre-post shaper
spectrum (shown in Figure 3-8) is the result of optics having different efficiencies for
transmission and reflectivity as a function of wavelength. The SLM-640 is the major loss
component of the shaper having ~40% transmission per propagation.
The native pulse width of an anamorphic focusing NOPA we built (or similar,
non-anamorphic NOPA) has not been previously reported. The 4-f compressor we built
combined with an SLM-640 allows a dynamic range of ~2 ps for temporal correction
(discussed earlier). Characterizing the native NOPA pulse to ensure it was shorter than
2 ps was performed with X-FROG, a frequency resolved crosscorrelation method
developed by Trebino10.
A BBO crystal has poor phase matching conditions when mixing wavelengths
that will generate a wavelength below 300 nm (the index of refraction of BBO becomes
non-linear bellow 300 nm). BBO cannot be used to autocorrelated the NOPA pulse
because 520 nm + 520 nm sum-frequency generates 260 nm (cannot be
autocorrelated). However, 520 nm + 800 nm sum-frequency generates 315 nm (just
above the cut off, allowing crosscorrelation). By mixing a pulse we could characterize
(800 nm fundamental) with a pulse we could not independently characterize, the
temporal profile of the NOPA pulse could be measured.
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Figure 3-9. Phase matching bandwidth for SFG between NOPA beam and 800 nm beam at various phase matching angles for 100 𝜇𝑚 thick BBO. A) Phase matching bandwidth at different angles of the BBO, B) illustration of how the phase matching angle is tuned to meet different phase matching conditions.
The NOPA spectrum + 800 nm bandwidth that can be simultaneously phase
matched at a single phase-matching angle of a 100 𝜇𝑚 BBO crystal is ~10 nm, meaning
only 10 nm of the NOPA spectrum could be phase matches to generate sum-frequency
at a single time. Figure 3-9A shows how much spectrum of the NOPA can be
simultaneously phase matches at a single BBO angle (experimentally collected data,
not calculated), each colored line corresponds to a different BBO angle depicted by
Figure 3-9B. Knowing that it is possible to phase match the whole NOPA spectrum at
different angles, allows to piecewise generate an X-FROG Trace of the entire NOPA
spectrum by changing the BBO phase matching angle between scans. A piece wise
generated X-FROG trace of the native NOPA pulse shown in figure 3-10 appear like
“islands” because it’s the addition of traces taken at different BBO angles. Figure 3-10A
shows the X-FROG trace of the NOPA pulse which travels through the 4-f compressor,
without the SLM in the Fourier plane. The temporal width of the native NOPA pulse is
measured at ~400 fs, well within the dynamic range of the SLM-640. Figure 3-10B
shows an X-FROG trace of the NOPA pulse after the SLM has been added in the
A B u
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Fourier plane, showing that the SLM adds a non-trivial phase distortion making the
pulse unworkable because it is spread out over more than 2 ps. The SLM-640 adds
more phase distortions than it can compensate. The non-trivial phase is a result of
deformations which are brought out by cylindrical focusing (discussed earlier). The
aberrations were characterized in detail by a previous student 30, which failed to
communicate that the aberrations in the mask are a significant problem.
A trick was used to compensate the phase distortions added by the SLM-640. By
purposefully miss-aligning the 4-f compressor, linear temporal chirp could be added to
compensate some of the distortions added by the SLM array. The linear chirp was
added by adding an angle to the folding mirror immediately after the grating (purple
optic in figure 3-6). Linear chirp was added, while monitoring the pulse width using X-
FROG, to achieve the shortest possible pulse without using SLM dynamic range. Figure
3-10C shows the compensated pulse is spread over ~1 ps, within the dynamic range of
the SLM-640.
The phase distortions we observe added by the SLM-640 are not the result of
material dispersion. We preform X-FROG measurements at the sample position, as
such, the timing convention is the same used for pump-probe spectroscopy. The NOPA
pulse is our “pump”, and the 800 nm we use for crosscorrelation is the “probe” (no white
light generation). If the pump arrives before the probe, time is positive; if probe arrives
before the pump, time is negative. From Figure 3-10B, the short wavelength (high
energy) components arrive at negative times, and the long wavelength (low energy)
components arrive at positive time, thus the dispersion by the SLM is positive (see
figure 3-11 for a simple illustration explaining the statement). Normal dispersion in a
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Figure 3-10. X-FROG traces of the NOPA pulse + 800 nm generated piecewise at
different BBO angles (discussed in text) showing that the SLM-640 destroys the phase
of a pulse. A) Native temporal profile of NOPA pulse, with no SLM in Fourier plane, B)
temporal profile after addition of SLM-640, C) compensated temporal profile after
temporal chirp was introduced.
Figure 3-10. X-FROG traces of the NOPA pulse + 800 nm generated piecewise at different BBO angles (discussed in text) showing that the SLM-640 destroys the phase of a pulse. A) Native temporal profile of NOPA pulse, with no SLM in Fourier plane, B) temporal profile after addition of SLM-640, C) compensated temporal profile after temporal chirp was introduced.
A
B
C
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medium always results in negative chirp (red wavelengths traveling ahead of blue
wavelengths) because the index of refraction of materials increases with shorter
wavelengths (increasing energy). The SLM is 2.45 mm thick, with only 0.02 mm of liquid
crystal thickness, majority of the thickness is BK7 glass and index matched epoxy. In a
double pass configuration, the chirp added by ~6 mm of BK7 glass leads to a temporal
delay of ~100 fs for NOPA spectrum from the shortest to longest wavelength.
Figure 3-11. Simple illustration to explain how we know the SLM-640 adds positive dispersion from an X-FROG Trace.
On a side note, Figure 3-11 can be adapted to explain why blue wavelengths
arrive first in TA experiments with white light as the probe, shown in Figure 3-12 (red
wavelengths travel ahead of blue in normal dispersion).
Figure 3-12. Simple illustration of why temporal chirp in a white light probe leads to blue TA signals arriving before red signals in time.
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Phase and Amplitude Control Using SLM-640
The first step in phase and amplitude control is calibrating the phase response of
the SLM-640 liquid crystal array as a function of voltage. A step-by-step explanation for
SLM-640 calibration is reported elsewhere.30 Each pixel in an array behaves differently
because of inhomogeneity, but we showed that that a single calibration curve can be
used to predict the phase response as a function of voltage for the entire array, with a
pixel-by-pixel correction factor.30
Once a calibration is in place, the following equations dictate the resulting phase
and amplitude of the pulse for a given frequency:
𝐴𝑆𝐿𝑀(𝜔) = |𝑐𝑜𝑠 (𝛥𝜑1 − 𝛥𝜑0
2)|
(3-1)
𝛷𝑆𝐿𝑀(𝜔) = (𝛥𝜑1+𝛥𝜑0)
2 (3-2)
The phase change added by each of the masks, Δ𝜑𝑖, can thus make a phase
only change if the same phase is applied to both mask, or amplitude only change if
opposite phase is applied to each mask.
To test the quality of a calibration, we generated double pulses (discussed later)
with delay 𝜏 separation from 0.1 fs to 2 ps. X-FROG measurements of the double pulse
showed no difference between the predicted delay and the measured delay, until after
~1 ps, where the phase required for double pulses started reaching the dynamic range
of the SLM. Some of the 2 ps Dynamic range is consumed to compress the pulse
(discussed later), prior to making double pulses.
Over the course of several years, the SLM calibrations only needed to be redone
after major events, such as an optic change in the 4-f compressor.
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Pump pulse compression
Given that the pump pulse has complex temporal chirp (see Figure 3-10C), the
phase needed to compress is determined empirically. A genetic algorithm (GA) written
by a previous student,30 used for pulse compression by optimizing a chosen feedback
parameter over the course of evolving generations. Choosing the proper feedback
parameter to evolve the generations is the most critical component of the compression
procedure. Maximizing the intensity of a non-linear signal is an ideal feedback signal
because the shortest temporal profile also has the highest peak intensity, yielding the
highest non-linear signal. The non-linear signals we tried are:
• Two-photon absorption
• SFG of Pump + 800 nm in BBO
• SFG of Pump + 800 nm in KDP
Each was unable to independently compress the pulse for distinct reasons which
will be discussed in detail.
Two-Photon absorption was performed using a photo-diode with a bandgap
larger than the pump wavelengths, but lower than the doubled wavelengths, allowing to
have response from multi-photon absorption events. The detector we used was based
on a SiC photo-diode design described elsewhere.32 Two-photon absorption was tried
first because it is a phase matching-independent non-linear signal. As discussed earlier,
BBO cannot phase match the entire pump spectrum simultaneously.
Two-photon absorption of the pump pulse was unable to serve as a feedback for
the GA because the temporal chirp of the uncompressed pump pulse yields no
detectible two-photon absorption. If the uncompressed pump pulse is taken to the
detector, the only signal measured is a baseline shift from heating. We know that the
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detector works because a partially compressed pulse (discussed later) gives a voltage
response on an oscilloscope with better signal-to-noise than detecting SFG from a non-
linear crystal on a commercial photo-diode (DET210, ThorLabs).
We had no choice but to use a phase matching-dependent signal to compress
the pulse.
SFG of Pump + 800 nm in BBO was attempted despite knowing that the whole
pump spectrum could not be simultaneously phase matched in a thin BBO crystal. We
quickly learned that phase matching the entire region of interest is critical and cannot be
avoided when dealing with complex pulses.
Figure 3-13. Crosscorrelation of Pump pulse + 800 nm pulse before and after a compression mask obtained with a GA using SFG in BBO is applied. A) Crosscorrelation taken using the same phase matching angle used for GA feedback, B) Cross Correlation taken using the next 10 nm increment of BBO phase matching angle, using a compression mask obtained at different phase matching angle.
Figure 3-13A shows a crosscorrelation of the pump pulse (blue) after a
compression using the same phase matching angle of the BBO used for GA feedback.
The uncompressed crosscorrelation (brown-dashed) is plotted simultaneously for
comparison of temporal profile and intensity between compressed and uncompressed.
Repeating the crosscorrelation with the same SLM phase mask, but changing the BBO
angle so the next ~10 nm of the pump pulse spectrum would phase match yields the
A A
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crosscorrelation shown in Figure 3-13B. Regions of the spectrum which don’t phase
match during the GA, are made worse by applying compression mask generated
without feedback in that region. The “best” pulse in Figure 3-13B has less intensity, and
is thus broader in time than the unshaped pulse. The temporal profile of the “best” pulse
in Figure 3-13B would appear shorter compared to the unshaped if the plot of the
crosscorrelation was normalized, the fact that the “best” is worse than unshaped is lost
without the intensity dependence. The two plots shown are for two adjacent phase
matching regions, separated by 10 nm of pump spectrum, the resulting “best” pulse is
even worse further in spectrum from the phase matching conditions used for GA
feedback. Phase matching the entire spectrum of interest is critical to pulse
compression.
Figure 3-14. Phase matching acceptance bandwidth of KDP (Blue) compared with BBO (Green) at a single crystal phase matching angle.
SFG of Pump + 800 nm in KDP. Potassium dihydrogen phosphate (KDP), is a
lesser known non-linear crystal compared to BBO in optical spectroscopy. KDP has
significantly better spectral phase matching acceptance bandwidth compared to BBO
when mixing 520 nm with 800 nm. KDP can simultaneously phase match the entire
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pump spectrum at a single-phase matching angle when mixing with 800 nm in a 100 𝜇m
crystal, as shown in Figure 3-14.
As discussed earlier, BBO can only phase match ~10 nm of pump at a single-
phase matching angle. KDP is ~500 times less polarizable than BBO and with a lower
damage threshold than BBO. KDP is only suitable for processes where the intensity of
the non-linear signal is not important, such as pulse characterization. Once a KDP
crystal was available, X-FROG characterization could be done in a single scan, instead
of piecewise in BBO (as discussed earlier).
Using the SFG signal generated in KDP as a feedback parameter for a pulse
compression allows for significant pulse improvement as seen in Figure 3-15. The “best”
pulse is not fully compressed however. There is wing structure with non-negligible
intensity, making the pulse unusable for a 2D-S experiment. The remaining wing
structure in the compressed pulse, can be related to the highly-structured part of the
uncompressed pulse (see X-FROG around SFG of at 320 nm in Figure 3-15).
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Figure 3-15. X-FROG and cross correlation of pump + 800 nm pulse before and after compression mask obtained with a GA using SFG in KDP is applied. A) X-FROG of unshaped pulse, B) crosscorrelation of best and unshaped pulse, C) X-FROG of best compression mask obtained from GA.
A
B
C
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Another trick was used to overcome the inability to simultaneously compress all
the wavelengths using SFG in KDP as feedback. The pump pulse is highly structured in
the long wavelength region as observed in X-FROG (see Figure 3-15A around 320 nm).
A compression GA can be biased to focus on the highly-structured region of the pulse
by blocking the pump spectrum in the Fourier plane for wavelength that generated SFG
signal above with shorter wavelength than 315 nm. Figure 3-16A shows the resulting
compressed pulse, by only focusing on the long wavelength component and blocking
shorter wavelengths. Phase masks are additive and can be mixed and combined, thus
the mask which compresses the long wavelengths, could be combined to the phase
mask which compresses the short wavelengths. Figure 3-16B shows the result of
combining to two phase masks, where one mask compresses the blue side and the
other the red side of the wavelengths. The semi-compressed pulses are short enough
for 2D-S experiments, but not ideal because the pulses have structure limiting the time
resolution of an experiment and making chirp correction in data harder because the
pump chirp needs to be deconvoluted from the probe chirp.
Compressed Pump Pulse. To achieve a compressed pulse, which is near-
transform limited, a pre-compressed pulse (shown in Figure 3-16B) was used as a
starting condition for a GA using two-photon absorption as feedback. Once a pulse is
short enough in time to generate two-photon absorption signal at all the wavelength
components of a pulse a the two-photon absorption detector sensitivity and improved
signal-to-noise can be used to remove the remaining structure and compress the pulse
to near-transform limited. The pulse characterized by X-FROG shown in figure 3-16C
cannot be used as a starting condition because the long wavelength region generates
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no two-photon response. Figure 3-17A shows an X-FROG trace of a compressed pulse
using two-photon absorption as feedback. A compression mask is usable for ~1-2
months. Figure 3-17B shows an X-FROG trace collected using the same compression
mask as figure 3-17A, but 6 months after the compression GA was run. As time passes,
a compression mask is no longer usable because the energy in the wings starts to
become a problem, as seen in comparing the baseline of the crosscorrelation in Figure
3-17C and Figure 3-17D.
Figure 3-16. Mixing compression mask can allow for pulse with better temporal profile than that achievable directly. A) X-FROG of Compression with the short wavelength region blocked, B) a mixed of the phase mask used for long wavelength compression and short wavelength compression, C) short wavelength compression used for part B.
A
B
C
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A crosscorrelation temporal resolution is limited by the longest of the two pulses
used. The X-FROG trace of the compressed pump pulse (shown in figure 3-17A)
measures a full width at half max (FWHM) of ~68 fs. X-FROG is achieved by mixing
pump pulse with an 800 nm pulse with ~64 fs FWHM (measured by autocorrelation).
This allows us to conclude that the pump pulse is shorter than 64 fs, because an
autocreation of two 64 fs pulses would measure ~90 fs (√2 ⋅ 64).
Figure 3-17. X-FROG and crosscorrelation of pump pulse + 800 nm pulse before and after compression mask obtained with a GA using two-photon absorption is applied. A) A compressed pulse near transform limited, B) drift in a compression mask collected ~6 months after GA was run, C) crosscorrelation of compressed and unshaped pulse, D) crosscorrelation of a pulse no longer suitable for experiments because of wings.
To fully characterize the pump pulse used for experiments, an interferogram was
measured by generating double pulses with the SLM and scanning over double pulse
delay using SHG signal. The resulting interferogram is shown in Figure 3-18. The lines
connecting the data points are not a fit, but straight lines to show the fringe pattern.
From the interferogram, we measured a pulse width for our pump of ~28 fs.
A B
C D i
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Figure 3-18. Interferogram generated by generating pulse pairs with the SLM-640 to generate a convolution spectrum. The lines are not a fit, they are lines connecting data points to emphasize the fringe pattern indicative of coherent pulse mixing.
It took 2 years after the 2D-S instrument was built to figure out all the problems
generated by the deformation of the SLM-640 and generate a compressed pump pulse
for 2D-S experiments. The SLM-640 is no longer sold for ultra-fast applications because
the added phase distortions from deformation render the unit essentially useless for its
intended purpose.
Double pulses
Double pulses can be generated through a phase and amplitude change on the
SLM such that the final field, �� 𝐹, becomes two identical clones of the original pulse, �� 0,
with a relative delay 𝜏, given by equation 3-3.
�� 𝐹(𝑡) =1
2(�� 0(𝑡 − 𝜏) + �� 0(𝑡))
(3-3)
The phase and amplitude mask, 𝑀(𝜔), needed to generate �� 𝐹(𝑡) is simple in the
frequency domain, given by equation 3-4 and 3-5. We introduce an arbitrary phase, 𝜙𝑖,
for each pulse in equation 3-4 because it is needed for phase-cycling (discussed later).
It is important to distinguish between the phase of a pulse, given by 𝜙𝑖, and the applied
phase of an SLM mask, given by Δ𝜑𝑖.
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𝑀(𝜔) =1
2(𝑒−𝑖𝜔𝜏+𝑖𝜙1 + 𝑒𝑖𝜙2)
(3-4)
�� 𝐹(𝜔) = 𝑀(𝜔) ⋅ �� 0(𝜔) (3-5)
In equation 3-5, 𝑀(𝜔) is a modulation mask, a term used in Fourier Theory to
describe a function to change one field into another. We use the SLM pixel array to
generate the mask, 𝑀(𝜔). Using Euler’s formula, equation 3-4 can be rewritten in a
form given by equation 3-6, that has a clear amplitude and phase component.
𝑀(𝜔) = 𝑐𝑜𝑠 (−𝜔𝜏+𝜙1−𝜙2
2) ⋅ 𝑒
𝑖 (−𝜔𝜏+𝜙1+𝜙2)
2 (3-6)
Looking back at equations 3-1 and 3-2, there is a simple solution to apply a
phase change on the SLM to generate a mask with the form given in equation 3-6.
Δ𝜑0 = −𝜔𝜏 + 𝜙1 (3-7)
𝛥𝜑1 = 𝜙2 (3-8)
The solutions shown in equation 3-7 and 3-8 are not unique, which SLM array
applies the 𝜔𝜏 term is invariant. However, the SLM pixel arrays are not equal, each has
a different amount of leakage (ability to apply desired phase). Figure 3-19 shows a 500
fs delay pulse pair measured by X-FROG generated by a 𝜔𝜏 phase change with
different SLM arrays. mask0 will generate a pulse with more intensity for the delayed
pulse (shown in Figure 3-19A), while Mask1 keeps more intensity at the non-delayed
pulse (shown in Figure 3-19B).
To see whether having different intensity pump pulses effects 2D-S experiments,
we collected 2D-S data for the molecule DASPI. One experiment, by making double
pulses with Mask0, and another with Mask1. The two 2D-S data sets were
indistinguishable, so further effort was put into the issue of pump pulse intensity.
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Figure 3-19. Difference in intensity of a pulse pair measured by X-FROG because of SLM array leakage. A) Pulse pair applied using mask0, B) pulse pair applied using mask1.
Broadband Seed/Probe Pulse
Figure 3-20. Typical white light spectrum generated in sapphire with different pump (800 nm) fluence. The fluence range shown is that for stable white light spectrums. The intensity is not normalized.
Broadband spectrum pulses are used for both seeding NOPA generation and as
a probe pulse for 2D-S spectroscopy. The broad band spectrum (white light) generated
in sapphire is pump fluence dependent, the range shown for stable spectral white light
generation in Figure 3-20. White light generation is a high-order non-linear process24
making generation very sensitive to the phase of the fundamental pulse. NOPA
generation becomes unstable if great care is not taken to generate a white light seed
with no detectible color difference in the beam except an intensity profile (seen by eye
A B
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on a cotton business card). The ability to control the focal point, fluence, and overlap in
sapphire of the 800 nm beam is critical to generate stable white light to seed the NOPA.
The optics used to generate the NOPA seed are described in chapter 2.
The white light probe is generated with a 3 mm waist beam of 800 nm focused
using a 25.4 mm focus round singlet lens onto a 2 mm thick sapphire window. The
sapphire window is uncoated with 𝜆/10 surface flatness and 10/5 scratch/dig (CVI). The
white light generated in sapphire is collimated with protected aluminum coated off-axis
parabolic mirror with EFL of 25.4 mm (ThorLabs, catalog number MPD019-G01). For
both NOPA seed and 2D-S probe, we specifically choose to generate the spectrum
shown with less fluence (Figure 3-20), because it allows for more wavelength range with
less chirp. Less chirp and more spectral range is a must to generate a broadband
NOPA pulse. However, the probe spectrum should be determined by the experiment. If
low wavelengths are not of interest, the spectrum generated with more fluence is more
stable in spectral intensity, improving signal to noise.
As mentioned earlier white light is very sensitive to the fundamental beams
phase stability. Air currents are enough to change the spectrum, phase and intensity of
the white light. It is important that the region around white-light generation is isolated.
Even with isolation the white-light generated has short (shot-to-shot) fluctuations and
long time (hours) fluctuations. The oscillations effect 2D-S data, because they add noise
to the Fourier Transform required for data processing. To help reduce the noise we use
self-referencing, where a part of the probe is split off with a beam splitter (thin wedge)
and propagates nearly the same path as the probe, except reaching a region of the
sample that is not excited by the pump (~1.5 mm separation at the sample). Self-
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referencing allows to distinguish between white-light oscillations from noise and
oscillations from 2D-S signal.
Pump-Probe Overlap
2D-S signal is generated when the pump and probe overlap in space and time.
The SLM controls the pump-pump delay (𝜏), and a commercial delay stage, DDS220
(ThorLabs) is used to control probe delay (𝑇). The reproducibility of the probe delay
stage is ~± 0.45 fs for a signal retroreflection configuration. Spatial geometry for overlap
was determined so a 10 cm by 10 cm footprint optical cryostat with 25.4 mm windows
could be places at the sample position. A long 15 cm EFL off-axis parabolic mirror
(OAPM) with a protected aluminum coating (Janos) is used for pump and probe overlap
to allow room for a large sample holder. The beams travel parallel to reach the OAPM
with a separation of ~6 mm and are thus focused at the same point without chromatic
aberrations. The beams travel with a small separation angle of ~2º to the sample
because of focusing. Focusing spots sizes were measured to ensure that the probe was
smaller than the pump, such that the probe did not detect any region of the sample not
excited by the pump. The probe spot size at the sample is 80 𝜇𝑚 and the pump spot
size is 170 𝜇𝑚 at sample, meeting the rule of thumb for pump-probe overlap (that the
pump be at least twice as large as the probe).
Sample Holder
Work done to bench mark our new instrument employed a liquid sample inside a
2 mm optical path length cuvette with a PTFE coated magnetic stir bar to prevent
thermal heating effects from the laser.
In the case of merocyanine-540 (MC540), stirring the solution was insufficient to
avoid detection of a long-lived isomer state (4 ms). Instead a commercial laser-dye
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pump (Spectra-physics) was used to flow solution through a home built flow cell with 2
mm optical path length. Cavitation from the pump was avoided using a gravity fed
reservoir with larger diameter feed tubing.
Measuring Signal
Once the 2D-S signal has been generated at the sample, it co-propagates with
the probe pulse (described in detail in chapter 2). A multi-core fiber with four individual
inputs and one output designed to place at the entrance slit of a spectrograph is used to
pick up the probe and reference beams after the sample (Andor, catalog number SR-
OPT-8027). AR coated fiber couplers were used to collect the beams into the fibers
(Newport, catalog number F-C5-S3-543).
The white-light beam has residual 800 nm and a fiber coupler has a tight focus,
thus the 800 nm left over has enough fluence to burn an optical fiber and/or generate
white-light in the fiber. A high-pass filter is required to remove wavelengths longer than
700 nm before entering the fibers, but after the sample. It is important to not filter 800
nm before the sample because, even a thin 1 mm filter will add a significant amount of
GVD to the white-light.
A CCD camera with 1300x1030 pixels (Roper, MicroMax 1300Y), and
spectrograph (Oriel, MS260i) were used to disperse the probe and reference into
frequency components to be measured. The CCD has a chip depth of 20 mm from the
face of the camera, and the spectrograph has an imaging length of 10 mm from the exit
slit, making it impossible to place the CCD at the correct location. Although the CCD
could not be used to image, it could be used to collect a spectrum which is what is
needed for 2D-S. Since the imaging points are not coincident, the wavelength
dispersion on the camera from the spectrograph is not linear at the chip position, thus a
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careful calibration is required. Four spectral lines are used for calibration, 3 from Hg-Ar,
and one from a He-Ne laser. Three points from Hg-Ar lines in the visible are not enough
points for a good calibration.
Instrument Control
Control of the instruments was achieved through a LabView interface. A program
was written by our group to allow coordinated control of the SLM-640, the probe delay
stage, the spectrograph, and the CCD camera. There are two independent parameters
in 2D-S, 𝜏 and 𝑇. The data can be collected by holding one parameter fixed, and
scanning all the 2nd parameter, then repeating for every value of the 1st parameter.
Which parameter, 𝜏 or 𝑇, is fixed while the other is scanned depends only on
experimental factors. It is better to scan 𝜏 and hold 𝑇 if a fast pulse shaper is used with
a slow stage. This procedure minimizes the number of times the stage needs to be
moved. In our setup, the pulse shaper is slower (response in seconds) so it is better to
scan 𝑇 and hold 𝜏. The current program scans 𝜏 and holds 𝑇, the next user can reduce
data collection time by modifying the program to scan 𝑇 and hold 𝜏. A non-trivial change
in the logic of the program, but worth the eventual saved time, a rough calculation
estimates that a 28 hour experiment (current average collection time) could be cut down
to ~18 hours.
Data Collection
Data collection must adhere to the Nyquist limit of the highest frequency
oscillation we want to detect. The high frequency edge of the pump pulse spectra is
~470 nm, which corresponds to a period of ~1.57 fs, thus a sample of Δ𝜏 = 0.784 fs is
required to overserve oscillation resulting from 470 nm excitation. The range of 𝜏 delays
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which needs to be measure is determined by the dephasing time of the system (needs
to be empirically determined, explained later). Data must be collected until the signal
decays—at least decays into the noise. Truncating a decaying oscillation leads to “sinc-
wiggles”, shown in Figure 3-21D, a well-known artifact in NMR. However, collecting
unneeded data past when the signal has decayed into the noise leads to a nosier 2D-S
plot, because baseline noise transfers into the FFT, as shown in figure 3-22. Before
collecting a full 2D-S data set on a new system, a scouting experiment must be
performed to figure out the range of 𝜏 that needs to be scanned.
Figure 3-21. Effects of truncating data and Hamming windows on the resulting FFT. Figure adapted from Ref 13.
A common method used to expedite the collection of data when only the peak
location matters and not the line-width, involves collecting less data than the range
needed to ensure the signal has decayed and using a Hamming window to force the
signal to zero to prevent sinc-wiggles, as shown in Figure 3-21E. Windowing the data
this way leads to broadening of the FFT, as shown in Figure 3-21F. Artificially
broadening the FFT leads to 2D-S plot that lose the physical meaning. A slice of 2D-S
Time Frequency
A B
C D
E F
FFTሱሮ
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data would no longer match an equivalent TA spectrum collected at the corresponding
excitation wavelength.
Figure 3-22. Effect of collecting unneeded data past the signal decay on the FFT signal-to-noise. Figure generated by James Keeler and reproduced with permission.
Improving Signal-to-Noise
The low signal intensities from 2D-S result in low S/N. Techniques have been
adopted to raise signal and reduce noise. One method proposed by Zanni, called
phase-cycling20 is based on the phase dependence of the 2D-S signal. It allows
distinguishing phase dependent from non-phase dependent processes, and removing
unwanted non-phase dependent signals. In pump-probe geometry the probe carries the
2D-S signal, as well as all other signals measured by the probe (i.e. TA and Raman).
Phase invariant signals, are noise in 2D-S Spectroscopy. The phase dependence of the
2D-S signal to pump phase can be explained by looking back to equation 2-10, and
introducing a phase dependence to the pump pulses given by the difference in phase
between the first and second pulse, Δ𝜙12:
𝑅(3) ∝ 𝑒𝑖Δ𝜙12 ⋅ 𝑒𝑖𝜔𝐵𝐴𝜏 ⋅ 𝑒−Γ𝜏 ⋅ 𝑒−𝑇𝜏𝐵
(3-9)
The phase dependence on the response, given by equation 3-9, results in a sign
change if Δ𝜙12 = 𝜋. Figure 3-23 shows the result of phase cycling a 2D-S experiment
with a Δ𝜙12 = 0 and 𝜋 pulse pair signal. The detected signal by a Δ𝜙12 = 0 scan (shown
Time
Frequency
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in red), can be subtracted from the signal generated by a Δ𝜙12 = 𝜋 scan (shown in
blue). The 2D-S response is equal for both experiments, but with opposite sign. The
transient absorption signal is phase invariant, so it remains the same. By subtracting the
two scans, the TA signal can be subtracted, and the 2D-S signals are additive, result of
subtraction is shown in green.
Figure 3-23. Phase cycling data shown in green results from subtracting signal collected with zero phase (red line), and difference in phase of 𝜋 (green line). Figure
reproduced from Ref 20 with permission of the PCCP Owner Societies.
The scheme used in our instrument is that suggested by Zanni,20 shown in
equation 3-10.
𝑆𝑃𝐶 = 𝑆(𝜙1 = 0, 𝜙2 = 0) − 𝑆(𝜙1 = 0,𝜙2 = 𝜋)
+𝑆(𝜙1 = 𝜋, 𝜙2 = 𝜋) − 𝑆(𝜙1 = 𝜋,𝜙2 = 0)
(3-10)
𝑆𝑃𝐶 represents the signal obtained by phase cycling. The scheme from equation
3-10, takes full advantage of the phase control provided by the SLM. In the article by
Zanni presenting phase-cycling,20 the claim is made that phase-cycling also removes
scatter because scattered light is not phase dependent. However, we discovered that
this method does not remove scatter, it only reduces it. The amplitude of a given
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frequency component in a pulse-pair is phase dependent, resulting in phase
dependence in the scatter. To understand, we need to go back to the modulation mask
applied to make double pulses with arbitrary phase 𝜙1 and 𝜙2 on the SLM, from
equations 3-1, 3-7 and 3-8. We get
𝐴𝑆𝐿𝑀(𝜔) = |cos (−𝜔𝜏 + 𝜙1 − 𝜙2
2)|
(3-11)
For Δ𝜙12 = 0,
𝐴Δ𝜙12=0(𝜔) = |cos (−𝜔𝜏
2)| (3-12)
The maximum amplitude for frequency 𝜔 occur at,
𝜏max = 𝑁 ⋅ 𝑇𝑝𝑒𝑟, (3-13)
with N being 0 and an integer, and 𝑇𝑝𝑒𝑟 the period of the frequency 𝜔. The amplitude is
zero when,
𝜏zero = (𝑁 +1
2) ⋅ 𝑇𝑝𝑒𝑟
(3-14)
For Δ𝜙12 = 𝜋,
𝐴Δ𝜙12=𝜋(𝜔) = |cos (−𝜔𝜏 + Δ𝜙12
2)|
(3-15)
𝐴Δ𝜙12=𝜋(𝜔) = |sin (−𝜔𝜏
2)| (3-16)
Thus, the amplitude of a frequency component (intensity available to scatters) will
oscillate as a cosine and sine pair between a signal collected with Δ𝜙12 = 0 and 𝜋.
When one is maximized, the other is zero. Scatter cannot be subtracted by phase
dependence because when one pulse pair has maximum scatter, the subtracted pulse
pair will have zero scatter at that frequency. Leading to an oscillation in the scatter
signal for each 𝜔 in a pulse pair, at its own frequency, which will get picked up by an
FFT. The scatter is wavelength resolved onto the CCD, so an individual pixel will only
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see scatter from the wavelength it corresponds to. The oscillation frequency will
oscillate at the same frequency of the scatter wavelength; thus, scatter will only appear
on the diagonal of 2D-S plot.
This is a significant advantage to TA, where scatter is detected everywhere that
scatter occurs. 2D-S allows systems with high scatter to be studied, limited only by not
being able to remove scatter from the diagonal. Intuitively it might seem like rotating the
frame of the 2D-S signal would eliminate scatter because the sampling frequency would
not match the frequency of the scatter, but this is not the case. Scatter will always follow
the relationship shown above, even if 𝜔 is shifted to 𝜔𝑟𝑓 = 𝜔 − 𝜔𝑖, the scatter will
appear at 𝜔𝑟𝑓 instead and still be on the diagonal of a 2D-S plot.
Data Processing and Management
Data sets are large 3D matrices, with a 𝜏 axis, 𝑇 axis, and 𝜆𝑑𝑒𝑡𝑒𝑐𝑡𝑖𝑜𝑛 axis. A data
file would be ~1.3 GB if data was saved in double precision as a text file with minimal
formatting. Time was spent to reduce file sizes such that our computers would not take
30 mins to import data files into MatLab. We focus on ease of data storage and
reducing the file size without reducing the information. The filetype we settled on is tab
delimited with the first line containing the dimensions of the 3D matrix, and the second
line containing all the elements of the matrix. This file is easy to import into MatLab by
using the commands:
>> fid = fopen('DataFile'); % opens the file (don't forget the extension and path)
>> arraySize = str2num(fgetl(fid)); % reads the first line
>> data = str2num(fgetl(fid)); % reads the second line
>> data = reshape(data,arraySize); % reshape the data into a 3D matrix
>> fclose(fid); % closes the file to clear space
Once the data was processed in MatLab, the results were saved as ‘.m’ files.
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New versions of LabVIEW allow MatLab to be run within the LabVIEW
environment, allowing the 3D data to be saved as a “.m” directly. The file type is very
efficient at storing matrices (e.g. a ‘.txt’ file in the format above would be ~100 MB, while
the same information in a ‘.m’ file already stored as a 3D matrix, with variable names
and headers would be ~40 MB). Some of our instrument drivers are not supported on
new LabView versions, so we could not directly implement this saving option.
The output of the data collection program is a differential transmission,
ΔT =Iprobe
𝐼𝑟𝑒𝑓𝑒𝑟𝑒𝑛𝑐𝑒− 1
(3-17)
The best instrument sensitivity will not be below a 1×10−6 Δ𝑇, which corresponds
to a Δ𝐴 of 0.4 𝑚𝑖𝑐𝑟𝑜𝑂𝐷. keeping only 6 decimal places of precision in our data files
greatly reduce the file size without loss of information.
Expectation Versus Reality
Looking back at Figure 2-23 and 2-24, the pump-probe 2D-S plots don’t match
with expectation from the concept of 2D spectroscopy when introduced in books or
lectures. We don’t observe well defined “blobs” of on/off-diagonal elements that show
coupling. In electronic 2D-S, there are many overlapping signals; making it difficult to
assigned signals to certain transitions. The advantage of 2D-S vs TA experiments,
includes the reduction of scatter as described earlier, and overcoming the limitation of
temporal bandwidth and spectral bandwidth of a pulse being coupled, Δ𝑡 ⋅ Δ𝜔 ≥ 2𝜋 ⋅
0.441 (for a Gaussian pulse). For example, a TA experiment cannot independently
excite and probe two transitions separated by less than the bandwidth of the pump,
because both states will be simultaneously excited. This is not a problem in 2D-S
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allowing for the possibility of observing coherent coupling between two similar
chromophores
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CHAPTER 4 MEROCYANINE-540
“If we spent more time doing experiments than making figures, we could change the world; but a good figure speaks a thousand words—”
Valeria D. Kleiman
Merocyanine-540 (MC540), as introduced in Chapter 1, has been studied for
over 40 years but the mechanism for isomerization and triplet state formation is still
elusive. Using the newly built 2D instrument we hoped to shed light into the excited
state dynamics.
Merocyanine-540 (MC540), shown in Figure 4-1, was designed as a molecular
probe to stain cells33. The functional groups of MC540 allow it to integrate into a lipid
membrane and to be soluble in both polar34 to non-polar35 solvents. The absorption and
fluorescence of MC540 are dependent on local environments, making it suitable for
probing micro-environments36 such as the charged surface of a nerve axon firing37.
Figure 4-1. Chemical structure of Merocyanine-540 in trans-isomer configuration, with red arrow showing carbon double bond assigned to rotation for cis-isomer configuration.
There are a few properties known about MC540, that have strong experimental
support: (1) MC540 forms aggregates in water,38 and dimers when on a lipid
membrane37, both aggregation and dimers are concentration dependent. (2) MC540
forms a triplet state upon visible light irradiation that can be quenched by saturating the
solution with oxygen.3 (3) In the ground-state at room temperature in ethanol, only one
isomer configuration of MC540 is detected by 2D-NMR.3 (4) A model system of MC540
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shows a similar TA spectrum when isomerized from trans to cis configuration, thus trans
configuration is assumed for MC540 in the ground state.39. (5) Isomerization and
emission are competing excited state deactivation pathways; if one goes up, the other
goes down and the ratio of the yields is temperature dependent.40 (6) the cis-isomer
absorption spectrum is red shifted and has a lifetime that depends on temperature.34 (7)
Solvent polarity greatly affects the isomerization rate and yield, but the values for
ethanol and methanol are similar.41
The seven properties listed above have strong experimental support. Pinning
down which carbon double bond isomerizes experimentally has been a matter of debate
for some time, but because cyanine is the chromophore of MC540, a large spectral shift
on the chromophore absorptions would not occur if an isomerization occurred at one of
the end double bonds. Working assumptions about MC540 will be based on the above
seven properties: from 7, methanol and ethanol have similar values for solvent polarity,
thus, considering point 3 and 4, we can assume that the trans-isomer configuration is
also the ground state in methanol. The highest isomer yield and lowest emission yield at
room temperature is observed in methanol34, making it the best solvent to look for a
spectral signature of excited state isomerization because overlap of signals is minimized
(explained below).
Overlapping Signals
Figure 4-2 show the transient differential absorption of MC540 10 𝜇𝑠 after
excitation3 in the top panels, along with the steady state absorption spectrum (blue line)
and emission spectrum (red line) in the bottom panels for comparison. Figure 4-2A and
4-2B show the differential absorption in a deoxygenated solution and oxygenated
solution respectively. The cis-isomer spectral signature (isolated in Figure 4-2B by
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quenching the triplet with oxygen) overlaps with the ground state bleach and expected
stimulated emission in a differential absorption experiment (i.e. pump-probe 2D-S and
transient absorption). Making it difficult to isolate excited state dynamics for different
species. Methanol was used in all our experiments to minimize the effect of overlap by
maximizing the isomer generation, and minimizing the overlapping stimulated emission
(red line).
Figure 4-2. Spectral signature of long lived transients top panel, 10 𝜇𝑠 after excitation with a 10 ns pulse of 532 nm. Normalized absorption (blue) and Emission (red) shown in bottom panel. A) Cis-isomer and triplet state spectral signatures in deoxygenated ethanol, B) cis-isomer spectral signature isolated in oxygenated ethanol. The top panels are reproduced from Ref 3 with permission of The Royal Society of Chemistry.
Method
Merocyanine at ~99% purity, purchased from ThermoFisher was used without
further purification. The solvent, Methanol, Extra Dry, 99.9% purchased from Fisher,
was further distilled to prevent water aggregates when doing experiments to observe
aggregates and the triplet state. After we established there was no triplet and no
aggregation (discussed later), HPLC grade methanol (Fisher) exposed to Florida
humidity without degassing was used for ultrafast experiments. Being able to use
A
B
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atmosphere exposed solvent was critical to allow a high flow cell (described in chapter
3) to avoid measuring MC540 long lived isomer signals (discussed later).
Steady-state absorption measurements were performed on a UV-VIS Jaz
spectrometer (Ocean Optics), and emission and excitation spectra were collected on a
Fluorolog-3 (Spex). When optical densities bellow 0.05 needed to be measured a Cary
50 Probe (Varian) UV-VIS was used. Steady state measurements were performed with
and without flowing comparing spectra we concluded the light sources for absorption
and emission were not intense enough to make any detectible amount of cis-isomer or
triplet for a steady-state measurement. Steady state absorption was collected for
various optical densities in a 2 mm cuvette. Steady state emission and excitation
spectra were collected with a 1 cm path length cuvette at ~0.005 OD sample to
minimize self-absorptions.
Throughout ultrafast experiments, a ~0.3 optical density sample was used. The
spot size of the pump for 2D-S experiments is measured at 170 𝜇𝑚 (beam waist) and a
pump energy of 20 nJ/pulse (10 nJ/pulse of a pulse pair) is used for excitation. We
measured 2D-S and TA up to 200 nJ/pulse (maximum without attenuation) without
observing non-linear absorption, but pump scatter needs to be considered because
scatter intensity transfers into TA and 2D-S data, settling on 20 nJ as a compromise
between signal intensity from the sample and noise from scatter intensity.
The pump-probe 2D-S instrument is home built with pump spectrum from 475 nm
to 565 nm and pulse width of ~28 fs (instrument described in chapters 2 and 3).
Transient absorption data was collected using a commercial TA instrument, Helios
(Coherent). The pump energy used for TA was 50 nJ/pulse, picked to match the fluence
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used for 2D-S. TA spot size was not measured, fluence was estimated by the focal
length and beam size.
2D-S data collection and processing is discussed in Chapter 2 and 3.
SVD/MCR-ALS: TA data was processed using singular value decomposition
(SVD) and multivariate curve resolution-alternating least squares (MCR-ALS)42 in
MatLab. SVD breaks a signal down to its basic components, or “eigen spectra”; if TA
data is the input, SVD will determine the minimum number of spectral components
needed to reproduce the TA data. Once the eigen spectra are determined, the TA signal
is fit using a linear combination of the eigen spectra, where the eigen spectra determine
the profile of the signal, and the time dependent constants (amplitudes) determine the
time evolution. Eigen spectra depend on the basis set used and SVD has no constraint
on the basis set leading to rotational ambiguity which means solutions are not unique
and often converge in a basis without physical interpretation. Finding the correct basis
set to show the eigen spectral components is achieved through MCR-ALS by applying
constraints to the SVD eigen components and amplitudes to conform to the physical
interpretation of the data. For example, non-negativity in the amplitude components
used for the linear combination is critical for TA data because TA spectral profiles can
have negative Δ𝐴(𝜆) values (i.e. ground state bleach and stimulated emission), but the
species generating the negative signal always has real and positive amplitude
(corresponds to the population of the state generating the spectral signal). Even if the
molecule absorbing the TA pulse is destroyed through the absorption of a photon
(photo-bond breaking for example) such that the ground state is not recovered, the
physical amplitudes will still be non-negative because the lack of recovery of the bleach
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is a spectral signature of the new species population. SVD and MCR-ALS cannot deal
with shifts in wavelength seen in TA and 2D-S from vibrational cooling and solvent
reorganization because each vibrational state gives a spectral signature different
enough to require its own spectral eigen component, and each vibrational eigen
component contributes so little to the overall signal (it rises and decays very quickly)
that the component is lost in the noise of an SVD fit.
Results
Steady-State
Merocyanine-540 is in a family of chromophores that is known to show
photodegradation over time. 2D experiments often take several days of continuous laser
excitation and detection to generate good S/N data sets because of the weak nature of
2D signals arising from a 3rd order weak perturbation. To ensure samples would not
photodegrade (or show no evidence) over the course of the experiment, a large volume
(~0.5 L) of dye was prepared to flow through the flow cell, and the absorption spectrum
of a sample from the reservoir was tested daily to ensure no detectable amount of
degradation.
Figure 4-3 shows the absorption spectrum (black) and emission spectrum (red)
of MC540 in methanol along with the pump spectrum (green) used in the 2D-S
experiments. The absorption spectrum (black line) has three bands/shoulders indicated
with arrows (determined by looking at the change in spectrum as function of wavelength
inflection points) with the maximum at ~555 nm, a band at ~518 nm the and a shoulder
at ~480 nm. The emission spectrum appears as a mirror image of the absorption,
indicative of similar Franck-Condon character of the ground state and excited state
vibrational states. The emission is red-shifted to absorption with a maximum at 580 nm.
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The pump spectrum (green) is the spectrum after pulse shaping (discussed in Chapter
3) and covers the three absorption bands/shoulders. The pump spectrum was
specifically chosen to have more intensity at short wavelengths components to ensure a
detectible 2D-S signal from the low absorption region of MC540.
Figure 4-3. Steady state spectra collected for MC540 in methanol. Absorption is shown in black, emission in red, and the pump spectrum used for 2D-S is shown in green
The excitation spectrum of MC540 was collected with detection at 600 nm
(negligible absorption from MC540) and at 660 nm to ensure that emission and
absorption had no excitation wavelength dependence. Figure 4-4 shows the excitation
spectra collected at 600 nm (blue) and 660 (orange) normalized to the absorption
spectrum (red dashed).
MC540 is reported to form dimers and aggregates in water.38 A dilution study of
MC540 was performed in wet methanol (HPLC grade methanol left exposed to high
humidity environment) to see if the water concentration would cause problems with
aggregation. Absorption spectra were collected at dilutions from 0.005 OD to 2.0 OD to
look for signatures of aggregations. Figure 4-5 shows the normalized absorption spectra
of the high optical density samples (where aggregation should be more apparent) with
Pump
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the unnormalized data shown below. For comparison, the absorption spectrum of
MC540 with optical density ~0.005 prepared in extra dry methanol (described earlier) is
superimposed (dashed black line) on the normalized spectra. From Figure 4-5 we can
conclude that “wet” methanol does not lead to aggregation, and from the extensive
range of optical densities we probed, if there is a dimer configuration in methanol it has
no observable concentration dependence in the limit of optical spectroscopy
concentrations.
Figure 4-4. Excitation Spectrum of MC540 in methanol with detection at 600 nm (blue) and 660 nm (orange). Sample optical density of ~0.005 OD in 1 cm cuvette was used. Spectra are normalized to absorption spectrum (dashed red).
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Figure 4-5. Dilution study of MC540 absorption prepared in atmospherically wet methanol. The top panel shows normalized absorption spectra collected in wet methanol, superimposed with the normalized absorption of MC540 prepared in extra dry methanol with ~0.005 optical density (black-dashed).
Long Lived Isomer
MC540 has a long lived cis-isomer with a reported lifetime of ~6 ms in methanol
at room temperature.3 The rep-rate of an experiment becomes a consideration when
measuring signals that persist longer than the time between excitation pulses (1 ms for
1 kHz laser). Figure 4-6 shows the TA signal observed before “time-zero” when stirring
is used to mix the solution (green). The signal measured is the difference between the
probe and reference signals because the sample in the vicinity of the probe pulse does
not have enough time to relax to the ground state trans conformation before the next
Concentration
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pump pulse arrives to re-excite the sample. The data in red shows the result of not
mixing the sample, bringing out the spectral signature of the cis-isomer reported in the
literature. The absorption spectrum is shown as a dashed black line for comparison,
along with pump pulse spectrum (20 nJ/pulse) used for TA as blue dashed line.
Figure 4-6. Transient signal detected before time-zero when the sample is not refreshed between pump pulses. Not stirring is shown in red and with stirring in green. Dashed lines are the absorption spectrum of MC540 (Black dashed) and pump spectrum with 20 nJ/pulse (blue dashed).
Starting a 2D-S or TA experiment with a combination of a ground state and
excited state increases the complexity of data analysis because the signals will overlap
and the ground state cannot be assumed.
Figure 4-7 shows TA collected before “time-zero” when using a high rate flow cell
(described in Chapter 3) to refresh the sample in-between laser excitations for 2D-S
experiments with no detectible difference between probe and reference. Figure 4-7A
shows one spectrum, and figure 4-8B shows spectra for many several times before
time-zero, to emphasize that the small off-set signal away from Δ𝐴 = 0 is not isomer
signal but an experimental artifact of not using a pump-off scenario to isolate differences
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between probe and references spectrum (2D-S does not need a pump-off case,
because the artifact is a “TA signal” which is subtracted by phase cycling).
Figure 4-7. Transient signal observed before “time-zero” when adequately refreshing sample between consecutive excitation pulses. A) One time before zero, B) many times before zero for comparison.
A home built optical cell and a commercial optical cell (Starna Cells, catalog
number 48-Q-2) were used for flowing experiments. Figure 4-8 shows the difference in
flow between the two, where the blue arrows are flow directions and the red arrow is
laser propagation direction. Both cell have a sample path of 2 mm. The home built cell
(Figure 4-8A) would flow the solution without a direction change, while the commercial
cell (Figure 4-8B) would flow the solution with a 90 degree turn. Use of the commercial
cell results in pump scatter picked up in an FFT of the data (discussed in chapter 3).
The pump scatter resulting from commercial flow cell is low enough to not be observed
on the detector, unless the probe light is blocked (only background noise) and the
averaging typical for experiments is used. We know the scatter results from the flow
direction and not the quality of the glass, because when the flow is turned off, no scatter
is observed. Time constraints left us not choice but to use the commercial cell for
experiments on MC540 when the home built cell became unusable from a solvent-
gasket mismatch that required replacement of all the components (note to future
A
B
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student, replacement parts are in the lab and the cell needs to be rebuilt). As such, 2D-
S data presented has scatter along the diagonal which is picked up as extra intensity on
the detector (negative Δ𝐴).
Figure 4-8. Solvent flow difference between home build flow cell and commercial flow cell used. A) home built cell flow leads to no scatter, B) commercial flow cell leads to scatter from flow path.
Two-Dimensional Spectroscopy
Experimental conditions are described in chapter 3 and in the methods section of
this chapter. All 2D-S plots of MC540 we present are normalized to the absorption
spectrum of MC540 allowing differences in excitation wavelength to be more easily
observed because the number of photons absorbed contribution to the signal intensity is
removed (equivalent to assuming, the sample absorbs the same number of photons at
every excitation wavelength, so the data can be read as “if photons are absorbed at
excitation… the system will show a response at the detection wavelength…”). Data
collection takes a long time (~30 continuous hours for the 2D-S presented here), and is
limited by how long the laser is stable. Therefore, non-uniform time steps for 𝑇 are used:
fine time delay steps for early times, to observer fast dynamics and larger steps with
longer delay time.
2D-S data for MC540 has fast early time (instantaneous to 4 ps) dynamics, that
is different from longer excited state dynamics (4 ps to 1 ns). The early and “long” time
dynamics will be discussed separately. At all times, there will be a negative signal on
A
B
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the diagonal (black line) arising from pump pulse scatter. Scatter does not decay with 𝜏
so there will be sinc wiggles around the scatter peak (see chapter 3) and scatter is not
constant, so it will change in intensity randomly in time and spectrum.
Three regions of the 2D-S plot will dominate the changes in the signal observed
over time, 𝑇. Figure 4-9 is one 2D-S plot (left panel) for 𝑇 = 0.3 ps, after solvent Raman
has dissipated, which will be used to explain what each region represents and how to
follow the data before we go into how the 2D-S signal changes in time. The right panel
shows the expected signals from the excited states of MC540 (where 2D-S signal
should appear). The horizontal axis is excitation wavelength, the vertical axis is
detection wavelength. A region of the plot can be read as “what is the signal observed
when exciting at 𝜆𝑒𝑥𝑐𝑖𝑡𝑎𝑎𝑡𝑖𝑜𝑛 and detecting at 𝜆𝑑𝑒𝑡𝑒𝑐𝑡𝑖𝑜𝑛”. As described in chapters 2 and
3, pump-probe 2D-S leads to absorptive signals so the intensity in the z-axis is a
differential absorption observed by the probe. The colors used to represent intensity on
the 2D-S plots are RGB for negative signals (less absorbed light means more light
reaching detector), and grey-scale for positive signals (more absorption means less light
reaching detector). This convention was chosen because positive signals give us little
information from the data we collect (except for very specific things which will be pointed
out), so emphasis is place on the negative signals with this color convention.
MC540 has maximum absorption at 555 nm (see figure 4-3), so we expect a
negative signal to be detected in this region from ground state depletion (purple in
Figure 4-9). The emission spectra of MC540 is maximized at 580 nm (see figure 4-3),
so we expect a negative signal from stimulated emission in this region (magenta in
Figure 4-9). From Figure 4-2 and 4-6, we can expect to see a positive signal from
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absorption of the cis-isomer (cyan spectrum in right panel) once it is formed around 580
nm detection, the same region as a negative signal from stimulated emission (cyan
circle in figure 4-9 shows the only region of the 2D-S data where the cis-isomer signal
will be detected).
Figure 4-9. 2D-S signal for MC540 at 𝑇 = 0.3 ps. Figure is described in text.
Early time 2D-S
Figure 4-10 shows the early time evolution of MC540 up to 4ps. The changes
observed, are: (1) an increase of negative signal detected at 580 axis, which appears as
a negative signal growing in the vertical direction; (2) a positive signal at early times
detected at 580 nm with excitation at 490 nm, quickly disappears in 1 ps and is replaced
by a negative signal; (3) The most intense negative signal (blue color) grows in size and
intensity and is not at the peak of the absorption spectrum of MC540 but at ~535 nm
excitation wavelength (this result requires spectral component analysis to separate
overlapping signals to understand, discussed later after TA experiments are preformed).
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Later time 2D-S
Figure 4-11 shows the later time evolution of the 2D-S signal. Two changes
dominate the signal: (1) intensity profile of the negative signal is shifting horizontally
along the excitation direction (use green color contour as a reference with purple guide
lines). The data is plotted vertically in time to emphasize the shift of the negative
absorption signal in excitation wavelength (leftwards along horizontal axis); (2) the peak
signal intensity of the negative signal (blue color) begins to decay. The 2D-S data is
hard to interpret and relate back to a physical process; the overlap of all the signals
make it difficult to conclude anything other than the excited state dynamics for MC540
are excitation wavelength dependent.
Our 2D-S data has too much noise to preform SVD and global fitting to isolate
overlapping signals. A TA experiment coincides to a vertical slice of the 2D-S data at
the same excitation wavelength. Therefore, three TA experiments were performed to
probe MC540 at the regions of interest observed from 2D-S. Excitation at 490 nm gives
a positive signal at early times where we expect the cis-isomer signature and excitation
at 517 nm and 555 nm absorption bands show different dynamic, so TA was also
performed at these wavelengths.
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Figure 4-10. Snap shots of the time evolution of the 2D-S signal of MC540 in methanol at early times. 𝑇 time of 2D-S plot is indicated in white in each panel.
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Figure 4-11. 2D-S data for later times of MC540 in methanol. Negative numbers are shown in color scale, and positive numbers in grey scale, with black set to zero; Black dashed line across is the diagonal. Grey vertical lines are guide lines to allow the shift in the excitation axis to be observed.
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Transient Absorption
Transient absorption data was desired at the three excitation wavelengths of
interest: 490 nm, 517 nm, and 555 nm. The three wavelengths collected were 480 nm
(easier to generate OPA with more stability), 515 nm (commercial instrument would
generate OPA centered at 515 nm when 517 nm was entered) and 555 nm. All three
excitation wavelengths were attenuated to a power of 50 nJ/pulse at the sample
position. TA was collected out to 4 ns, with steps size of 0.5 ps until 1 ns, and 2 ps
steps until 4 ns. As discussed earlier, SVD cannot fit a shift in spectrum, which we
observe in 2D-S at early times (see Figure 4-10 for detection around 590 nm). We know
this signal to be vibrational cooling from previous time resolved emission studies.43
Once complete data sets for each excitation wavelength were collected with high S/N,
SVD was performed to isolate overlapping signals. Figure 4-12 shows a TA spectrum of
data collected at 480 nm excitation to give an idea of the quality of TA data needed to
get excellent fits acquired from SVD/MCR-ALS analysis (next section).
Figure 4-12. TA data collected for MC540 in methanol with excitation at 480 nm (blue arrow). Each spectrum is a 5 ps step starting at (red) to 4 ns (blue). Pump scatter is blocked in the spectra shown.
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SVD / MCR-ALS
SVD is tricky to understand because it looks like TA data, someone familiar with
TA but not SVD, might confuse a spectral component with a TA spectra, and an
amplitude temporal evolution with a kinetic trace of a TA spectrum at a single
wavelength. If you skipped the method section of this chapter and are not an expert in
SVD, please go back and read parts concerning SVD and MCR-ALS, before this
section. TA data after 5 ps was used for SVD (after vibrational cooling has finished).
Figure 4-13 shows the results for SVD using the TA data collected at 555 nm
excitation. There are only 2 significant spectral components. Meaning two eigen spectra
can be used to reproduce the data set with minimal error deviation from the data. All
three TA data sets at different excitation wavelengths had only two significant spectral
components.
Figure 4-13. Singular Value Decomposition values of TA data for MC540 in methanol excited at 555 nm. Inset shows all singular values of the TA data matrix.
MCR-ALS was used to place constraints on the SVD spectral components, to
show the components in a basis which would allow physical interpretation
corresponding with TA experiments. The only constraint used was non-negativity in the
spectral amplitudes (see Appendix if it is not clear why), so that spectral components
could not change sign (discussed in methods), only decay and/or rise. We also forced
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the optimization to continue until the error improvement was less than 0.01 percent
between iterations; the default error convergence is 1%. Increasing the convergence
constraint was critical because we noticed that two convergence runs would result in
spectral components with different spectral profile and amplitude evolution, even though
the error between the MCR-ALS fit was less than 1% error with TA data. Once the
convergence constraint was raised, all three TA data sets converged to the same two
spectral components shown in Figure 4-13A. Although all three TA data sets share the
same two spectral components, though the time evolution of the corresponding
amplitudes is quite different. Figure 4-13B shows the time evolution of the first spectral
component, for the three different pump wavelengths, which are color coded. Figure 4-
13C shows the time evolution of the second spectral component, for the three different
pump wavelengths. The black curves are fits of the data (discussed later).
Using only the two eigen spectra shown in Figure 4-14, along with their amplitude
components as a function of time, the TA data sets can be reproduced with no structure
in the residuals when the data is subtracted from the fit for all the wavelengths detected
in TA, from 450 nm to 700 nm. Figure 4-15 shows the residuals for all times and
wavelengths after 5 ps when SVD fits of 555 nm are subtracted from raw the raw TA
data. Only residuals for 555 nm excitation is shown because it is the nosiest data set.
The two spectral components from SVD/MCR-ALS were assigned as a cis-
isomer species (red from Figure 4-15A.), and an excited state species (blue from figure
4-15A). The assignment was straight forward considering component I (red) is the only
signal after 1.5 ns and matches the profile of the spectral signature of the cis-isomer in
solution in literature3 (see Figure 4-2B), and we observe the same spectral signature
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after 1 ms if care is not taken to refresh the sample volume between excitations (see
figure 4-6).
Figure 4-14. Spectral components and spectra from MCR-ALS for TA data collected at three different excitation wavelengths along with multi-exponential fit (black curve). A) Two significant spectral components from MCR-ALS, B) time evolution of red component at three different excitation wavelengths, C) time evolution of blue component at three different excitation wavelengths.
Figure 4-16 explains the composition of each SVD/MCR-ALS spectral
component shown in Figure 4-15A. A simplified Jablonski diagram is included above the
spectrum to help explain the spectral signatures of having population in an excites state.
Figure 4-16A shows the spectral component assigned to the isomer species which is
the spectral signature (differential absorptions) of having population in the cis-isomer
state. The profile will include ground state bleach (missing absorption because some of
A
C B
I II
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the molecules are in the cis-isomer configuration, and not absorbing like the trans-
isomer), and the cis-isomer absorption (a new positive absorption resulting from the cis-
isomer having a different absorption spectrum than the trans-isomer). The predicted cis-
isomer spectrum (dashed line) is obtained by subtracting the profile of the ground state
absorption of MC540 (solid black line) from the SVD component. Figure 4-16B shows
the composition of the excited state species spectral signature. The spectral profile
observed from having populating in the excited state will include a ground state bleach
(explained earlier), stimulated emission (a negative signal because more photons reach
the detector), and excited state absorption (a positive new absorption because the
excited state can absorb into another excited state). The predicted excited state
absorption shown in Figure 4-16B is generated by using the MC540 absorption and
emission spectra as the bleach and stimulated emission and subtracting from the SVD
component obtained from Figure 4-14A (assuming equal oscillator strength for ground
state absorption and stimulated emission).
Figure 4-15. Residuals from TA data excited at 555 nm fit using the SVD/MCR-ASL results shown in Figure 4-15.
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Time evolution
The kinetic profiles of the spectral components obtained from SVD/MCR-ALS
were fit using a sum of exponentials which are the fits shown in black in Figures 4-14B
and 4-14C. The least number of exponentials needed to avoid structure in the residuals
was used. The lifetimes are found in Table 4-1, along with amplitude components
reported as a percentage of total signal.
Excitation at 515 nm can be fit with one exponential for fitting both SVD
components with no structure in the residuals. The excited state decay of 515 nm
excitation could be fit by 257 ps (±1 ps) lifetime, outside of those values, residuals
would have structure, while the isomer rise could be fit with 270 ps (±30 ps) without
structure in the residuals. 257 ps is inside the range that can fit the rise with no
residuals, so 257 ps was assigned for both 515 nm comports. The tight tolerance of 257
ps, led us to use this value for other excitation wavelengths when possible.
Excitation at 480 nm could also be fit with a single exponential sharing the
same rates used for 515 nm with no structure in the residuals. The difference is that
both are decay times.
Excitation at 555 nm required at least two rates to fit the data. Fitting time
constants when more than one exponential is involved can be tricky, because there is a
large tolerance range for rates and amplitude combinations which will give rise to a
good fit with no residual structure. A judgment call is needed to help constrain the range
of rates and amplitudes, keeping in mind the potential for physical interpretation, and
always trying to minimize the number of free variables.
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Figure 4-16. Composition of spectral signitures of SVD/MCR-ASL components. Black line is the absorption spectra of MC540 in methanol. Dashed line is predicted excited state absorbtion. Dash and dotted line is emission spectra of MC540 in methanol. A) Cis-isomer component composition, B) excited state component composition.
A B
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The common lifetime from 480 nm and 515 nm of 257 ps, was used for 555 nm
pump wavelength data to constrain the second rate. The isomer state component is
easy to fit with an additional fast rise. The excited state can tolerate a second
component from 25 ps to 100 ps, a vast range for a small number. Which is chosen
would significantly affect the amplitude of the rates. We choose to report a lifetime of 30
ps because the physical interpretation is easier if the excited state feeds the cis-isomer
state (as one decays, the other rises).
Table 4-1. Lifetimes and amplitude percentages of SVD/MCR-ALS components. Excitation wavelength
[nm]
Excited state lifetime [ps]
Cis-isomer state lifetime* [ps]
480 257 +12/-24 100% 257 +4/-8 100%
515 257 ±1 100% (257) +33/-17 100%
555 257 fixed 30 +70/-5†
89% 11%
(257) fixed (30) +3/-3
55% 45%
* Long lived cis-isomer component not included. † Strange error explained in text. Note: Numbers in parenthesis are rise times.
Discussion
Using SVD/MCR-ALS to isolate overlapping spectral features facilitates
interpretation of the 2D-S data. The shift along the excitation axis in Figure 4-11
detected at 580 nm is the result of signal with positive Δ𝐴 contribution decaying for
excitations around 480 nm, while a signal with positive Δ𝐴 contribution rising faster at
555 nm excitation than at the center. The time resolution of the TA experiment (1 ps)
could not help to determine the character of the positive signal observed at early 2D-S
times, however, TA data supports the idea that the cis-isomer spectral signature forms
in less than 5 ps.
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Ultrafast Formation of Cis-isomer Spectral Signature
Ultrafast isomerization8 processes have been observed before, but MC540
isomerization has not previously been reported to occur on the time-scales we observe
for excitation at 480 nm, probably because no one thought to excite the molecule there.
Using the information from 2D and TA, we began to construct a model that would fit
these new findings and agree with previous data. To start, we suspected a surface
crossing or conical intersection was involved near the Franck-Condon region because
of the fast time scales observed in isomerization. MC540 is a large molecule and cannot
be modeled using a method that could accurately predict the Franck-Condon region
(absorptions spectra) and the excited state surfaces (conical intersections and surface
crossings), so we were limited to smaller model systems for insight.
Unfortunately, no simple model (and not so simple models) can explain
everything we observe. If we only needed a model to explain each of the excitations
independently, it would be trivial, but kinetics for excitation at 515 nm can’t be explained
by the models for 480 nm or 555 nm, or vice versa. We are missing a piece of the
puzzle to bridge the difference in kinetics between different excitation energies, but we
don’t know what that is. All the excited state population is accounted for in the two
spectral signatures from SVD/MCR-ALS. We know this because a dark state which
gave no spectral signatures other than a ground state depletion, would require its own
spectral component to fit the data (the signature of missing absorption of the grounds
state). SVD/MCR-ALS data matches the TA data with less than 1% error, which means
if we are missing a spectral component, less than 1% contributes to the transient
signals.
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Every kinetic model for MC540 we could find in literature fails when attempting to
explain the excitation wavelength dependence we observed. A model that cannot
predict an experimental result is wrong, so a new model is needed.
Excitation wavelength dependent cis-isomerization yield? The instantaneous
detection of the cis-isomer spectral feature with excitation at 480 nm, and the faster
formation kinetics when exciting at 555 nm, compared to 515 nm, made us wonder if the
yield of the isomer was also excitation wavelength dependent. Emission is said to
compete with isomerization, so if the cis-isomer forms faster in some cases, the yield
can be expected to change. All the TA experiments were performed with the same
pump power, so the SVD/MCR-ALS results were normalized to the corresponding
absorption spectrum value (isolating the signal from optical density). The result being
normalized data independent of number of excited molecules. Figure 4-17 shows the
normalized cis-isomer component amplitude kinetics. The result of normalization shows
that the same amount of cis-isomer forms after ~1 ns, regardless of the excitation
wavelength. Combing this information with the lack of excitation wavelength
dependence of emission (discussed earlier) makes it a truly puzzling problem; there are
starkly different excitation wavelength dependent kinetics, but with the same overall
yields after all the excited state kinetics are settled.
Merocyanine-540 has proven to be a complicated system eluding even a
complex model able to explain all the observed behavior. Our research hoped to add
pieces to the puzzle to shed light on this curious system with real world importance, but
instead we discovered that the puzzle is bigger than previously imagined.
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Figure 4-17. Normalized cis-isomer component amplitude kinetics for 3 different excitation wavelengths.
Complicating things further, the well documented triplet state of MC540 was not
detected in our experiments, despite extensive efforts to try to observe it.
Triplet State
Not observing the triplet state in methanol, made us question our methods and
results, because its spectral signature and kinetics are heavily reported in literature.
After we finally convinced ourselves that our methods were valid by observing triplet
states in other systems, we did a deep literature search to figure out why we were not
measuring a triplet state. Having published work for over ~40 years of intense study on
MC540, made it possible to conclude that a triplet state is only measured, if the pump
power is high44,45 and the pulse width of the excitation source is long, above 100’s of ps.
We were not able to find a short pulse experiment with experimental evidence of
the Triplet. A single ultrafast paper by the Kamat group46 mentions the triplet, but their
ultrafast data is cut off starting at the wavelengths where triplet signature is expected.
The spectrum of the triplet they report to observe was collected using a 532 nm pulses
555 nm
480 nm
515 nm
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with 6 ns temporal bandwidths and 10 mJ/pulse, not an ultrafast pulse. Every single
other paper that mentions the triplet state of MC540 (with experimental evidence, and
not just a reference to another paper) uses a CW laser, nanosecond laser, or
microsecond flash photolysis to discuss the triplet state.
Not measuring a triplet state with short pulses is compelling evidence that the
triplet state is the result of re-excitation of something other than the ground state. This
might be a way to finally settle the debate of whether MC540 kills leukemia by triplet
formation or isomerization. An ultrafast laser can be used to excite live leukemia cells
stained with MC540 in such a way that the same cell isn’t re-excited until well after the
cis-isomer has decayed. The laser would need to have a low rep-rate to allow for gentle
methods of displacing the sample from shot-to-shot, or the position of the laser pulse
from shot the shot can be changed using acoustic displacement of an optic to change
the focal position from shot-to-shot.
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CHAPTER 5 CONCLUSION
"A good experimentalist doesn't mean being able to collect beautiful low-noise data; it means when you measure something you don't expect you’re able to distinguish
whether there is mistake in your experimental methods or a mistake in the theory." Adrian Roitberg
Two-dimensional spectroscopy in the optical electronic region for pump-probe
geometry experiments is not yet a mature scientific method. The problems that plague
transient absorption (overlapping signatures of species) are also present in optical 2D-
S. Something that is neglected to be explained when the “amazing things which 2D-S
can show” part of a lectures, presentations, journal articles, and books is covered.
Signals overlap in 2D-S and TA spectroscopy, so SVD is used to figure out
independent components to isolate the kinetics of individual species (see Chapter 4
methods). SVD results have ABSOLUTLY no physical meaning without
constraining the basis set. Eigen components of a matrix only have physical meaning
if they are shown in a basis set with physical meaning. However, 2D-S fits using SVD
component analysis are justified in literature with global fitting of decay associated
spectra, to show that the SVD results “fit the data well”. If the SVD components didn’t
fit the data well, they would not have been picked up by the algorithm to
reproduce the data set—a good fit does not mean anything other than the 2D-S
data set has noise tolerable for the algorithm to converge on some non-unique
solution. Having a good fit of data is not science, because any unconstrained function
with unlimited parameters can reproduce data with a “good fit”. Except for things that
can’t be fit like random signals and chaotic behavior, but those are their own “beasts”.
Constraining 2D-S data from SVD to have physical meaning using MCR-ASL is
very challenging; SVD does not work on 3-D data sets, so slices of the 3-D matrix must
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be done separately. 2D-S data is also much harder to collect than TA, making
generating a data set with low noise and enough time points for SVD analysis very
difficult. To compound the complexity of interpreting data, lots of the interesting
dynamics of systems occur on time scales where vibrational states are still “hot”,
meaning SVD cannot be used to separate overlapping signals; unless data set with
enough time and temporal resolution is collected for “hot” vibrational states to be
represented in the data long enough to not be considered noise by the algorithm.
Making 2D-S data have physical meaning, should be the top priority for the
optical 2D-S community, kinetics and fits discussed for data which might have no
physical interpretation is troubling.
Tensor decomposition47 (SVD in 3-D) is a promising method currently in
development which might allow optical 2D-S data to be processed to extract species
information from overlapping signals. Up to now, no successful application has been
used on data as complex as 2D-S data. However, the “deep-learning” community is
heavily interested in tensor decomposition because computers use SVD to break down
images; not being able to look at the time-evolution of images (i.e. movie, or real-time
visual input) prevents computers from interpreting time-dependent signals such as
understanding what action is being performed over time. The large amount of resources
being invested into deep-learning will hopefully lead to the development of a tensor
decomposition algorithm which can be used for 2D-S data.
There is significant advantage to a 2D-S experiment compared to a TA
experiment (discussed in Chapter 3). 2D-S will eventually replace TA as technology
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advances because of the advantages, just as FT-IR is now the standard for vibrational
spectroscopy.
My contribution to the field was not building a new instrument that could perform
experiments no one else can (yet, a publication to help others access the blue-green
region of the visible spectrum for pump-probe 2D-S is in the works), or showing that
MC540 is an even more complicated system than what was previously known; my
contribution to the field is showing that pump-probe 2D-S measures real signals that
can be interpreted with fits corresponding to physical processes. The difficulty of the
experimental method and theory is not an acceptable excuse to not explain what the
signal means—if you can collect data, but not understand what it means, you’re a
skilled technician, not a scientist.
Merocyanine-540 Excited State Kinetics
The excitation wavelength dependence of the excited state dynamics of
merocyanine-540 (MC540), observed using 2D-S in the pump-probe geometry and
confirmed by TA experiments, described in Chapter 4 cannot be explained by any
current model of excited state MC540 in the literature. The trouble arises from observing
faster cis-isomer formation signature at both high energy (480 nm) and low energy (555
nm) component of the absorption spectrum.
Adding to the complexity is the lack of excitation wavelength dependence on
emission and cis-isomer yield. Accounting for starkly different dynamics while
maintaining emission yield and isomer yield with only two species with two rates
(extracted from SVD/MCR-ALS), is daunting for a kinetic model. Another complexity is
MC540 vibrationally cools in ~4 ps after excitation, from time resolved emission
studies43 and shifts observed in our data. The additional 30 ps rate for 555 nm excitation
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compared to 515 nm, cannot be explained from being exciting to different vibration
states, because both should be in the same vibrational state after ~4 ps.
An extensive literature review on MC540 and similar molecules was performed to
see if similar dynamics have been previously observed.
Figure 5-1. Transient data for a model merocyanine which shows spectral signatures like those observed for merocyanine-540. Figure adapted with permission from Kahan, A.;
Wand, A.; Ruhman, S.; Zilberg, S.; Haas, Y. Solvent tuning of a conical intersection: direct experimental verification of a theoretical prediction J Phys Chem A 2011, 115, 10854-10861. Copyright (2011) American Chemical Society.
A simple merocyanine model (MCM), shown in Figure 5-1A, shows similar
kinetics to what we observe for MC540, except the differences in kinetics are from
different solvents, instead of different excitation wavelengths.9 Figure 5-1C shows the
TA spectra of MCM in toluene and Figure 5-1D in acetonitrile with spectra color coded
to time, and absorption spectrum (dashed line) and emission spectrum (dotted line) for
D
C
B
A
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comparison. Figure 5-1B shows the kinetic profiles at 660 nm detection color coded to
solvent.
The molecule MCM does not form a trans-cis isomer in the ground state because
isomerization around the double bonds yield no difference, and the central bond is
unrestricted. From calculations on a similar simple merocyanine without the tertbutyl
moieties, the first excited state is predicted to be a zwitterion.48 The Valence Bond
theory calculation, assignments are shown in Figure 5-2. Combining the TA results
shown in Figure 5-1, with the calculated VB assignments, the excited state spectral
absorption signature around 660 nm, is assigned to the zwitterion excited state
absorption by Haas.48
Figure 5-2. VB structure used to assign transition from work by Haas on the MCM system. Figure reproduced with permission from Kahan, A.; Wand, A.; Ruhman, S.; Zilberg, S.;
Haas, Y. Solvent tuning of a conical intersection: direct experimental verification of a theoretical prediction J Phys Chem A 2011, 115, 10854-10861. Copyright (2011) American Chemical Society.
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It’s a stretch, but applying the idea that the spectral signature of an excited state
zwitterion form has similar spectral profile as a ground state cis-isomer of MC540, it is
possible to assign some of the different kinetics observed for MC540 at different
excitations, to whether a zwitterion forms. The temporal response we observe between
different excitation could be a result of an overlapping zwitterion excited state
absorption signal. From figure 5-3B, amplitude profiles for the 480 nm excitation
component (blue) could be explained if lots zwitterion populations formed, and the
decay we observe is the decay of the zwitterion signal convoluted with the rise of the
isomer signal. The spectral profile of the signal assigned to cis-isomerization state in
Chapter 4, could be a mixture of cis-isomer absorption, and excited state zwitterion
absorption with profile so similar that they are mixed by SVD/MCR-ASL, and the kinetics
of the components keep track of the species, instead of the profile.
Figure 5-3. Reproduction of plots shown in Figure 4-15.
I purposefully choose to neglect zwitterions through the dissertation because
zwitterions predicted for MC540 is one of the properties discussed in Chapter 1, where
it is mentioned in literature so often that is assumed to be true. Tracking references
down to find an experiment which shows MC540 forms the zwitterion configuration, lead
to papers that are speculative about the possible formation of a zwitterion without any
555 nm
480 nm
515
ground state bleach
cis-isomer/zwitterion absorption?
A
B
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experimental evidence. Refence chains for mentions of zwitterions of MC540 often end
at an article34 for which the evidence for a zwitterion presented is being able to draw a
resonance structure. An undergraduate chemist learns in physical chemistry that a
resonance structure does not mean that the two species will exist, only that the true
conformation is a combination of both. And indeed, the true ground state has some
zwitterion character, as discussed in interpretation of 2D-NMR experiments to
determine the ground state conformation.3
Complicating things even further when trying to see if there is experimental
evidence or at least strong tangential support reaches the problem of the “hot topic”
nature of zwitterions in the 90’s. Like how someone will have trouble when doing a
literature search for keyword “nano” for publications in the 2000’s. On top of being
difficult to research for directly in literature, MC540 is often clumped in work with other
similar dyes that make no mention of merocyanine. This means that there might be
convincing evidence somewhere, and I just can’t find it.
Zwitterion Evidence?
It is possible we generated experimental evidence of a zwitterion configuration
accidently by exciting at 480 nm, while looking for signature of the isomer. An elaborate
experiment would need to be performed to confirm the results.
2D-S/TA Experiments with other solvents would need to be performed. The
excited state vibrational band which couples to the zwitterion state can’t be assumed to
be the high frequency band like that is observed for MC540 in methanol. The surface
crossing location is dependent on polarity not the vibrational structure, so the absorption
band which couples is expected to shift around with solvent properties.
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The surface crossing with a zwitterion is also predicted to shift with the
application of an external field48, allowing to stay with methanol because of the
favorable properties discussed in Chapter 4 for transient spectroscopy.
Looking at the problem with a background in physics, I would look for anisotropy
of the emission when excited at 490 nm, in varying external fields; the charge separated
state would want to align with the field. However, I have never done anisotropy
experiments and I only know the basic theory and not whether the experiments would
be possible on MC540 and methanol (high polarity solvent). The lack of emission yield
from excitation spectra shows that if the zwitterion exists it must fluoresce, or relax back
down to the state which emits to conserve the overall yield. Looking for a change in
anisotropy when applying an external field compared to anisotropy when exciting at a
wavelength with different kinetics would be evidence of a zwitterion.
Another experiment to probe for a zwitterion configuration would be to do 2D-
S/TA experiments with a visible wavelength pump pulse and IR wavelength probe
pulse. The vibrational signature of a charge separated species should be significantly
different form a neutral excited state-conformer because a polar solvent should perturb
the vibrations and shift the frequencies.
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APPENDIX CONSTRAINING SVD
Constraining SVD results using MCR-ALS in MatLab is a significant part of data
analysis to ensure that the correct kinetics are being reported and discussed. The
kinetics of a SVD fit without putting the eigen spectra into a proper basis set leads to
confusion and erroneous results which do not relate to physical processes. Pump-probe
geometry 2D-S measures observables with physical meaning: the system is put into a
coherence by the first pump pulse; the coherence evolves for time 𝜏 after which the
second pump pulse puts the system into a population state. The population state
evolves for time 𝑇 until the third pulse arrives and puts the system back into a
coherence; the coherence is not allowed to evolve and is immediately measured by
heterodyning the third-order signal with the third pulse (probe) on the detector. The
signal measures purely absorptive signals as discussed in Chapter 2.
To observe the excited state signals generated by 2D-S and TA, measurements
are presented as a differential absorption by subtracting the absorption of the pure
ground state. As a result, when population is in an excited state, a bleach signal is
always present; if the negative signal expected for a bleach is not observed, it means
that it is masked by a positive signal (excited state absorption) with a larger oscillator
strength at the same spectral range.
Relating SVD results to a physical signal being measured has been a topic of
debate in the literature. Pre-packaged software for SVD analysis, such as KOALA and
MCR-ALS have many available constraints to change the basis set of an SVD fit to
have physical meaning. The constraints available to end-users of SVD analysis
software can be confusing, and it is critical that SVD analysis not be treated as a “black-
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box” method to analyze data. If you do not understand what SVD does to a data matrix
and what it means to change the basis of a matrix, you should not use SVD—the results
are meaningless unless the correct constraints are applied.
Non-negativity of the amplitude components is a critical constraint for SVD
analysis so TA and 2D-S data have physical meaning. However, this constraint makes
TA very difficult to analyze because of experimental noise and spurious signals (i.e.
solvent Raman and pump scatter). Requiring the data to be high S/N and spurious
signal free is probably the reason that prevented others from realizing how simple it is to
extract information from overlapping TA signals. As a species approaches zero Δ𝐴
(decaying back to ground state) the noise of a measurement will result in the measured
signal oscillating from positive to negative amplitudes (see Figure A-1A of an
exponential decay (red) with 10% RMS noise data (blue)). The negative amplitudes
prevent SVD analysis to fit the data well because a non-negative amplitude constraint
was applied. Figure A-1B shows the results of fitting data using a non-negativity
constraint (orange). High, one sided residuals (between a fit and data) result from being
unable to generate negative amplitudes to match the experimental data.
Pump scatter and Raman are not TA signals from the sample and are thus not
associated with a population of an excited state. To use SVD on TA data, the data set
must be low noise and spurious signals free such that when the error from being unable
to produce negative amplitude values is negligible.
Some examples of excellent “fits” of MC540 TA data presented in Chapter 4 (see
Figure 4-12) with no physical meaning are shown in Figure A-2. TA measures the
spectral signature of having population in the excited state. The excited state population
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will yield both positive and negative Δ𝐴 signals (bleach, stimulated emission, and
excited state absorption); the eigen spectra need to be free to be both positive and
negative. However, the amplitudes of the spectral components represent the population
of the excited state generating the spectrum measured by TA; populations must be non-
negative, so the amplitudes must be non-negative. TA measures differential absorption,
thus, if the bleach does not recover because the ground-state population is not
conserved (i.e. bond breaking), it does not mean there can be a negative population for
the ground state, instead it will be measured as a positive population of a species
whose spectral signature is a lack of ground state absorption.
A caveat for anyone attempting to reproduce my results is the following: MatLab
generates “initial guesses” each time the program is started and reuses the same
numbers until the program is restarted. Running the same unconstrained SVD/MCR-
ALS optimization back-to-back will yield the same results. To generate a new non-
unique solution, close and restart MatLab, then rerun the optimization. Different runs will
converge on different results because the initial guesses are different and SVD
solutions are not unique when unconstrainted. Data shown in Figure A-2 was generated
by two consecutive runs of unconstrainted SVD/MCR-ALS analysis of MC540 TA data
shown in Figure 4-12.
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Figure A-1. Example of a decaying exponential signal with noise. Figure explained in text.
A
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Figure A-2. Two unconstrained fits of MC540 TA data that fit the data well, but have no physical meaning. A) amplitudes change sign from positive to negative (bottom panel, orange line), B) fit showing that meaningless spectra and amplitudes can fit data well.
B
A
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LIST OF REFERENCES
1. Ben-Bassat, H.; Goldblum, N.; Manny, N.; Sachs, L. Mobility of concanavalina receptors on the surface membrane of lymphocytes from normal persons and patients with chronic lymphocytic leukemia. International Journal of Cancer 1974, 14, 367-371.
2. Sieber, F.; Spivak, J. L.; Sutcliffe, A. M. Selective killing of leukemic cells by merocyanine 540-mediated photosensitization Proc. Natl. Acad. Sci. U. S. A. 1984, 81, 7584-7587.
3. Benniston, A. C.; Harriman, A.; Gulliya, K. S. Photophysical properties of merocyanine 540 derivatives Journal of the Chemical Society, Faraday Transactions 1994, 90, 953.
4. Atzpodien, J.; Gulati, S. C.; Clarkson, B. D. Comparison of the Cytotoxic Effects of Merocyanine-540 on Leukemic Cells and Normal Human Bone Marrow Cancer Research 1986, 46, 4892-4895.
5. Vilpo, J.; Vilpo, L.; Group, T. C. Selective toxicity of vincristine against chronic lymphocytic leukaemia in vitro. The Lancet 1996, 347, 1491-1492.
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BIOGRAPHICAL SKETCH
Jorge I. Medina received his Ph.D. in chemistry under the mentorship of Valeria
D. Kleiman at the University of Florida in the spring of 2017. His undergraduate
education was performed at California State University, Long Beach, where he obtained
a B.S. in physics and astronomy in the spring of 2009.