the effect of transverse shifts on the ligo interferometer doug fettig - oregon state university...
DESCRIPTION
ICGC-2004, Kochi, India 3 Transverse Shifts Figure 1 shows the interferometer in the normal operating state or the unperturbed state. Figure 2 shows the interferometer in a perturbed state where all the mirrors have been shifted in the x- direction by 1cm.TRANSCRIPT
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The Effect of Transverse Shifts on the LIGO The Effect of Transverse Shifts on the LIGO InterferometerInterferometer
Doug Fettig - Oregon State UniversityMentor: Biplab Bhawal
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ICGC-2004, Kochi, India 2
Purpose and Motivation
Purpose Through computer simulations I will map the
response of the interferometer to various transverse shifts in the optics.
Determine how these shifts will effect the detector’s performance.
Motivation It is believed that one of the input mirrors at the
Hanford observatory is misaligned by 1-2 cm. Also, the laser beam, at times, has been shifted on
the order of 1 cm.
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ICGC-2004, Kochi, India 3
Transverse Shifts
Figure 1 shows the interferometer in the normal operating state or the unperturbed state.
Figure 2 shows the interferometer in a perturbed state where all the mirrors have been shifted in the x- direction by 1cm.
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Comparison of Simulation Tools
End-to-End (e2e) Time domain simulation
package. SimLIGO is a good
description of the LIGO detector with detailed models of the optics, suspension system, noise sources, wavefront and length sensors, etc.
Relatively Long simulation time.
MIT FFT Code Frequency domain
simulation package. Gives a very accurate
description of the interferometer in the steady state.
Static simulation that doesn’t simulate feedback corrections.
Relatively short simulation time.
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Transverse shifts are equivalent to rotations
Rotation about the x-axis is known as pitch. If the mirror is offset by 1cm in the Y-direction, a pitch of 0.01/R radians is needed to counter the shift, where R is the radius of curvature for that mirror.
Similarly, rotation about the y-axis is called yaw (notice the sign difference between the two).
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Comparison of angles
Example of Rotation: If R = 7500m, then a 1cm shift would produce equivalent yaw (or pitch) of
Divergence angle: 1 x 101 x 10-5-5 radians radians
A calculation by Fritschel suggests that a misalignment of 1 x 10-8 radians should result in a 0.5% increase in shot noise.
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Wavefront sensors: Misalignment signal
Signal 0 <=Signal 0 <=
Signal non0 <=Signal non0 <=
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FFT simulation
In FFT I used the parameters and specifications to model LIGO Hanford’s detector. In this simulation I shifted the 5 mirrors, Recycling, ITMX, ETMX, ITMY, ETMY, by 1cm in the x direction.
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FFT: Results from a 1cm Shift in all mirrors
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Sideband Comparison at ITMX backside
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Interferometer’s Response to Shifts
To stay in a resonant and locked state, the mirrors of the interferometer must rotate to counteract the 1cm shift.
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e2e Run: Shift in All mirrors
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Sensitivity/Noise Curve
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Concluding Remarks
Through my investigations this summer, I was able to diagnose some errors in the simulation programs.
The independent simulation packages gave coinciding results, which adds some credibility to the simulations.
Many of the results obtained agree with prior predictions made about how transverse shifts should affect the interferometer.
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Acknowledgements
Special Thanks to
Biplab Bhawal Ken Libbrecht LIGO/SURF
NSF