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The Use of Vector Magnetogram Data in MHD Models of the Solar Atmosphere and Prospects for an Assimilative Model George H. Fisher Space Sciences Laboratory University of California, Berkeley

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The Use of Vector Magnetogram Data in MHD Models of the Solar Atmosphere and Prospects for an Assimilative Model. George H. Fisher Space Sciences Laboratory University of California, Berkeley. What would an ``Assimilative Model’’ of the solar atmosphere consist of?. - PowerPoint PPT Presentation

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Page 1: George H. Fisher Space Sciences Laboratory University of California, Berkeley

The Use of Vector Magnetogram Data in MHD Models of the Solar Atmosphere and Prospects for an

Assimilative Model

George H. Fisher

Space Sciences Laboratory

University of California, Berkeley

Page 2: George H. Fisher Space Sciences Laboratory University of California, Berkeley

What would an ``Assimilative Model’’ of the solar atmosphere consist of?

A time-evolving physical model of the Sun’s atmosphere, or a portion of the Sun’s atmosphere, which can be corrected by time-dependent measurements that can be related in some manner to properties of the solar atmosphere.

In particular, this means a 3D-MHD model of the Sun’s atmosphere, from photosphere to corona, that is updated by means of vector magnetograms.

Page 3: George H. Fisher Space Sciences Laboratory University of California, Berkeley

What are the most important elements of a physics-based model of the Sun?

• Nearly all transient phenomena, such as solar-initiated “space weather” events, are driven by, or strongly affected by, magnetic fields.

• A fluid treatment (MHD) is reasonable most of the time (except, probably, during solar flares).

• Magnetic fields thread all layers of the Sun’s convection zone and atmosphere.

• Maps of the estimated solar magnetic field (line-of-sight component) can be performed regularly in the photosphere.

• In the near future, maps of all 3 components of the estimated magnetic field (vector magnetograms) will be taken regularly.

• Vector magnetograms are essential for determining the free energy available in the solar atmosphere to drive violent phenomena. Without vector magnetograms, solar models are not meaningfully constrained.

Page 4: George H. Fisher Space Sciences Laboratory University of California, Berkeley

This Diagram taken from Welch and Bishop (2006) “An introduction to the Kalman Filter”

A is the physical model time-advance operatorH operator relates state variable x to observable zK is the Kalman filterQ is estimated process or model errorR is measurement errorP is estimate of state variable error

Schematic diagram of an assimilative model employing the Kalman filter approach:

Page 5: George H. Fisher Space Sciences Laboratory University of California, Berkeley

Needed ingredients for an assimilative (e.g. Kalman filter) model of the solar atmosphere:

1. A reasonably good physical model2. Measurements with a good enough time

cadence and accuracy to be useful3. A well-understood connection between

physical and measured variables4. A good understanding of the data and

model errors

Where do we stand with respect to these requirements?

Page 6: George H. Fisher Space Sciences Laboratory University of California, Berkeley

1. What are the minimum requirements for a “reasonably good” physical model?

• The model must accommodate the range of conditions from the photosphere, where magnetic fields can be routinely measured, into the corona, where ``space weather’’ events occur

• The model must include the dominant terms in the energy equation that apply in the photosphere-corona system. The dominant terms are drastically different in the different parts of the domain

• The model must be able to accommodate the wide range of physical and temporal scales from the photosphere to the corona.

• The model must be able to accommodate vector magnetic field maps, as a time-dependent boundary condition. This is required whether or not the model is truly assimilative!

Until recently, no existing models satisfied these requirements.Here is a brief summary of the challenges:

Page 7: George H. Fisher Space Sciences Laboratory University of California, Berkeley

Numerical challenges:

A dynamic numerical model extending from below the photosphere out into the corona must:

• span a ~ 10 - 15 order of magnitude change in gas density and a thermodynamic transition from the 1 MK corona to the optically thick, cooler layers of the low atmosphere, visible surface, and below;

• resolve a ~ 100 km photospheric pressure scale height while simultaneously following large-scale evolution (we use the Mikic et al. 2005 technique to mitigate the need to resolve the 1 km transition region scale height characteristic of a Spitzer-type conductivity);

• remain highly accurate in the turbulent sub-surface layers, while still employing an effective shock capture scheme to follow and resolve shock fronts in the upper atmosphere

• address the extreme temporal disparity of the combined system

Page 8: George H. Fisher Space Sciences Laboratory University of California, Berkeley

The Solar Photosphere

Hinode is a Japanese mission developed and launched by ISAS/JAXA, with NAOJ as domestic partner and NASA and STFC (UK) as international partners. It is operated by these agencies in co-operation withESA and NSC (Norway)

The solar photosphere is an extremely thin, corrugated, and complex layer, in which the plasma β in strong field regions is of order unity. This is the layer in which magnetic fields can be measured most routinely.

Page 9: George H. Fisher Space Sciences Laboratory University of California, Berkeley

Movies courtesy of LMSAL, TRACE & LASCO consortia

The solar corona:• The corona is a low-density, low-β, optically-thin, hot plasma

• Plasma entrained within coronal loops evolves rapidly compared to sub-surface structures

• The magnetically-dominated corona can store energy over long periods of time, but will often undergo sudden, rapid, and dramatic topological changes as magnetic energy is released.

• The size scale of coronal structures is generally much larger than the depth of the photosphere

Page 10: George H. Fisher Space Sciences Laboratory University of California, Berkeley

Qpet

et

B

Bp

t

t

2

2

4

48

0

Buu

BBuuB

gΠBB

Iuuu

u

RADMHD (Abbett, 2007, ApJ, in press): Numerical techniques

• We use a semi-implicit, operator-split method.

• Explicit sub-step:Explicit sub-step: We use a 3D extension of the semi-discrete method of Kurganov & Levy (2000) with the third order-accurate central weighted essentially non-oscillatory (CWENO) polynomial reconstruction of Levy et al. (2000).

• CWENO interpolation provides an efficient, accurate, simple shock capture scheme that allows us to resolve shocks in the transition region and corona without refining the mesh. The solenoidal constraint on B is enforced implicitly.

Page 11: George H. Fisher Space Sciences Laboratory University of California, Berkeley

Qpet

et

B

Bp

t

t

2

2

4

48

0

Buu

BBuuB

gΠBB

Iuuu

u

RADMHD: Numerical techniques

• We use a semi-implicit, operator-split method

• Implicit sub-step:Implicit sub-step: We use a “Jacobian-free” Newton-Krylov (JFNK) solver (see Knoll & Keyes 2003). The Krylov sub-step employs the generalized minimum residual (GMRES) technique.

• JFNK provides a memory-efficient means of implicitly solving a non-linear system, and frees us from the restrictive CFL stability conditions imposed by e.g., the electron thermal conductivity and radiative cooling.

Page 12: George H. Fisher Space Sciences Laboratory University of California, Berkeley

Characteristics of the Quiet Sun model atmosphere:

Note: Above movie is not a timeseries!

Page 13: George H. Fisher Space Sciences Laboratory University of California, Berkeley

Velocity determination at the photosphere for magnetogram-

driven modelsCurrently, we have been exploring driving the RADMHD code directly with sequences of vector magnetograms, without using any assimilative techniques. To do this, it is necessary to find the velocity field at the photospheric boundary, such that it is consistent with the vertical component of the magnetic induction equation. We have spent a lot of effort deriving and evaluating techniques to do this, with our leading techniques being MEF (Longcope et al) and ILCT (Welsch et al).

In addition to its importance for driving the code, these techniques are useful on their own to derive Poynting and helicity fluxes directly from magnetogram observations.

Page 14: George H. Fisher Space Sciences Laboratory University of California, Berkeley

An example of magnetic evolution in an active region

• NOAA AR 8210, May 1 1998 – 1 day of evolution seen by MDI

Page 15: George H. Fisher Space Sciences Laboratory University of California, Berkeley

Local Correlation Tracking

• Central idea of LCT schema: find proper motions of features in a pair of successive images are by maximizing a cross-correlation function (or minimizing an error function) between sub-regions of the images.

• The concept is generally attributed to November & Simon (1988).• Useful with G-band filtergrams, H images, or magnetograms.

• The FLCT method (which we developed) is similar. For each pixel, we: – mask each image with a Gaussian, of width , centered at that pixel;– crop the resulting images, keeping only signficant regions;– compute the cross-correlation function between the two cropped

images, using standard Fast Fourier Transform (FFT) techniques; – use 2nd order Taylor expansion to find the shifts in x and y that

maximize the cross-correlation function to sub-arc-second precision; and

– use the shifts in x and y and t between images to find the intensity features' apparent motion along the solar surface.

Page 16: George H. Fisher Space Sciences Laboratory University of California, Berkeley

Example of FLCT applied to NOAA AR 8210 (May 1 1998)

Page 17: George H. Fisher Space Sciences Laboratory University of California, Berkeley

The Demoulin & Berger (2003) Interpretation of LCT

Apparent horizontal

motion, ULCT , is from

combination of hori-

zontal motions and

vertical motions acting

on non-vertical fields.

zz

LCT VB

B

VU

Page 18: George H. Fisher Space Sciences Laboratory University of California, Berkeley

The Ideal MHD Induction Equation• How can we ensure that LCT-determined velocities are physically consistent with the magnetic induction

equation?

• Only the z-component of the induction equation contains no unobservable vertical derivatives:

)()(

Bv zzz Bt

Bv

0)(

zz Bt

BU

zzz BB v BvU

Now, substitute in the Demoulin & Berger hypothesis

The ideal MHD induction equation simplifies to this form:

Page 19: George H. Fisher Space Sciences Laboratory University of California, Berkeley

I+LCT (ILCT): Use LCT to constrain solutions of the induction equation

• Solve for , with 2D divergence and 2D curl (z-comp), and the approximation that U=ULCT:

.zvBU zzz BvBLet

2

t

Bz 2 LCTzUB

Note that if only Bz (or an approximation to it,

BLOS) is known, we can still solve for , !

Page 20: George H. Fisher Space Sciences Laboratory University of California, Berkeley

Apply ILCT to IVM vector magnetogram data for AR 8210

• Vector magnetic field data enables us to find 3-D flow field from ILCT via the equations shown on the previous slide. Transverse flows are shown as arrows, up/down flows shown as blue/red contours.

Page 21: George H. Fisher Space Sciences Laboratory University of California, Berkeley

2. Measurements of the magnetic field at the photosphere

Slide courtesy of Tom Metcalf, CoRA/NWRA

Page 22: George H. Fisher Space Sciences Laboratory University of California, Berkeley

How is the vector magnetic field determined?

• Magnetic fields will be split by Zeeman effect, but using the split itself not useful in most cases.

Spot in 5250 A (normal Zeeman triplet)

Slide courtesy of Tom Metcalf, CoRA/NWRA

Page 23: George H. Fisher Space Sciences Laboratory University of California, Berkeley

Zeeman Effect: Normal Zeeman Triplet

• Pi component is unshifted in wavelength (1)

• Sigma components shifted to either side of pi component (2).

• If the magnetic field is directed along the line of sight, the sigma components are left and right circularly polarized and the pi component is unpolarized.

• If the magnetic field is directed perpendicular to the line of sight, the sigma and pi components have mutually orthogonal linear polarizations.

σ

σ

π

Slide courtesy of Tom Metcalf, CoRA/NWRA

Page 24: George H. Fisher Space Sciences Laboratory University of California, Berkeley

How is Polarization Measured?

• Polarization is measured as the difference between data obtained using two different polarizers.

• For example a Wollaston prism or a calcite beam splitter produces two output beams of orthogonal linear polarization: I+Q,I-Q.

• U and V follow in the same way with a retarder in the path.

Slide courtesy of Tom Metcalf, CoRA/NWRA

Page 25: George H. Fisher Space Sciences Laboratory University of California, Berkeley

The Stokes Profiles• A magnetograph

observes the Stokes profiles.

• V/I is circular polarization and gives the LOS field

• U/I and Q/I are linear polarization and give the transverse field

Slide courtesy of Tom Metcalf, CoRA/NWRA

Page 26: George H. Fisher Space Sciences Laboratory University of California, Berkeley

Observed Stokes Profiles

• Na-D line observations from the IVM• They look more or less as expected with a few differences:

– Noise is clearly present– prefilter distorts spectrum

Stokes I Stokes Q Stokes U Stokes V

Relative Wavelength (nm)

Slide courtesy of Tom Metcalf, CoRA/NWRA

Page 27: George H. Fisher Space Sciences Laboratory University of California, Berkeley

3. Relationship between observed and measured variables - inverting the

polarization observations

• With the polarization in hand, how do we compute the magnetic field?

• There are a number of methods– Direct measurement of line splitting– Fitting Stokes profiles– Weak field approximations– Calibration constant(s)

• Different methods actually measure different quantities: the magnetic field or the flux density. Beware the difference!

Slide courtesy of Tom Metcalf, CoRA/NWRA

Page 28: George H. Fisher Space Sciences Laboratory University of California, Berkeley

Inverting the Polarization Observations

• The best method is to observe the Zeeman splitting directly.– Not generally possible for optical observations since the

fields on the Sun are too weak.– The Zeeman splitting goes as so this works better in the

IR.– Gives the magnetic field directly without worrying about the

filling factor.• The next best method is to fit the Stokes profiles to the Unno

profiles (Milne-Eddington atmosphere: source function linear with optical depth).– This gives the magnetic field, filling factor, thermodynamic

parameters

2

Slide courtesy of Tom Metcalf, CoRA/NWRA

Page 29: George H. Fisher Space Sciences Laboratory University of California, Berkeley

The 180 Degree Ambiguity• The observed transverse field is ambiguous by 180 degrees.• There are a number of ways to fix this but, as a practical matter,

this is most difficult for the most interesting regions and easy for uninteresting regions.– Acute angle solution

• Fast, will fail in complex active regions– Minimum energy solution

• Very slow, but more robust– Correspondence with H-alpha fibrils

• Generally accurate, but difficult to automate

Slide courtesy of Tom Metcalf, CoRA/NWRA

Page 30: George H. Fisher Space Sciences Laboratory University of California, Berkeley

4. Known sources of error in vector magnetograms:

• Photon statistics

– Polarization is computed as a difference of two signals

• polarization cross talk

– Polarization signal “leaks” between Stokes parameters

– Is corrected on an instrument-by instrument basis

• calibration constant

– The calibration constant in magnetographs is very approximate and is not constant at all.

• atmospheric seeing

– Will induce spurious polarization, sometimes strong

• polarization bias

– Should be correctable in most instruments by looking at the continuum or regions of very weak field.

• bad 180 degree ambiguity resolution (how to quantify??)

Bottom line – vector magnetogram errors can be characterized, at least statistically Slide courtesy of Tom Metcalf, CoRA/NWRA

Page 31: George H. Fisher Space Sciences Laboratory University of California, Berkeley

Summary of assimilative model requirements

1.Reasonably good physical model – good progress!

2.Measurements with good time cadence, accuracy – rapidly improving!

3.Well-understood connection between physical variables and measurements – reasonably good

4.Understanding of data errors – reasonably good; understanding of model errors - unknown

Page 32: George H. Fisher Space Sciences Laboratory University of California, Berkeley

Issues that must be resolved for an assimilative solar MHD model

• Currently, the data are used directly to determine the flow-field at the photosphere. How can this be made consistent with the Kalman “corrector” step, since the data have already been used?

• Can the Kalman filter approach be used in a “sub-step” process to determine the photospheric velocity field instead of using the ILCT or MEF procedures?

• Noise in the vector magnetogram data will probably introduce spurious Alfven waves into the model, even with the “filtering”. How do we cope with this?

• How do we estimate “model” errors?

Page 33: George H. Fisher Space Sciences Laboratory University of California, Berkeley

Conclusions

• Difference between assimilative and models directly driven by data (such as we are now performing): Assimilative models have the potential to accommodate data errors more consistently

• Assimilative techniques are worth detailed investigation for solar MHD models.

• There are other, simpler solar models that may be more immediately amenable to assimilation techniques.