Analysis of sensitivity and noise sources for the Virgo gravitational wave interferometer
Author: Supervisors:
Scuola Normale Superiore di Pisa
G. Vajente prof. F. Fidecaro prof. L. Foà
Pisa, May 21th 2008
Summary
Introduction
Interferometric detection of gravitational waves Virgo
Longitudinal control of Virgo
Brief description Characterization
Noise sources
Linear noise projection technique Discussion of Virgo noise budget after the first science run
Analysis of noise non-stationarity
Monitoring of band-limited RMS Linear regression analysis Short transient detection
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Introduction
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Interferometric detection /1
Gravitational waves generate a differential distance change between free falling masses Interferometers are very sensitive instruments
h
L
L
10
21
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Interferometric detection /2
Michelson interferometer at dark fringe: the field recombination at the antisymmetric port is destructive
LASER
Beam splitter: semi-transparent mirror
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Photo-detector
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Interferometric detection /3
Michelson interferometer at dark fringe: the field recombination at the antisymmetric port is destructive The amplitude of output signal is proportional to length and to circulating power
LASER
Gravitational waves creates a differential phase shift in the two arms
Interference is no more destructive A signal can be detected
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Resonant cavities
Techniques to increase the detector sensitivity to GWs
Fabry-Perot resonant cavities: arms replaced by resonant cavities to increase the optical gain (dephasing / equivalent displacement) Power Recycling: light reflected back to symmetric port is recycled by a semi-transparent mirror, to increase circulating power
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The Virgo interferometer
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Virgo design sensitivity
h ~ 3 x 10-21 Hz-1/2 @ 10 Hz h ~ 7 x 10-23 Hz-1/2 @ 100 Hz
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Seismic isolation
Super-attenuators: multi-stage passive seismic isolation system
MODEL
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Actuation system
Force is applied
To the mirror using coil/magnet pairs and a reaction mass suspended to the same seismic isolation system To the marionette: using coil/magnets pair and the upper suspension stage as reaction mass To the uppermost stage of the super-attenuator (Filter 0) with coil/magnets, from ground
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Last two stages of the super-attenuator
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Longitudinal control
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Longitudinal control
Mirrors relative distances must be kept fixed in order to maintain correct resonant conditions inside the cavities
CARM is equivalent to lWE laser frequency change Mean length of arms is used to stabilize laser frequency
l NI lWI PRCL l PR 2 MICH l NI lWI CARM l NE lWE 2 DARM l NE lWE
lNE lNI
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lWI
lPR
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Feed-back control systems
Seismic motion
Optical system (plant)
Error signal
Actuator
Correction signal
Control filter (corrector)
Error signals for the longitudinal control are extracted from interferometric beams with a frontal modulation technique
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Pound-Drever-Hall technique
Field is phase-modulated RF sidebands are reflected by the cavity
RF sidebands do not enter the cavity They are (almost) insensitive to cavity length They can be used as fixed phase reference
Aeit
Aeit eim cost
EOM
Resonant cavity
~
Error signal sensitive to cavity length change
Photo-detector
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Longitudinal control topology
MICH
8MHz
CARM PRCL
DARM
6MHz
6MHz Gabriele Vajente – Analysis of Sensitivity etc. – May 21st 2008
FREQ
6MHz 16
Characterization of longitudinal control
Adding a suitable external pertubation to a feed-back system it is possible to measure transfer functions The feed-back loop change the signal response The goal is to extract the optical response from the measurement
Seismic motion
Optical system (plant)
Error signal
Actuator
Correction signal
Control filter (corrector)
External perturbation
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Characterization of longitudinal control
In the Virgo case the system is multidimensional 4 degrees of freedom It can be solved using linear algebra The result is the optical response of photo-diode demodulated signals to MICH / PRCL / DARM / CARM displacements
Optical matrix
Driving matrix
Sensing matrix
Control filter matrix
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An example: dark fringe response
Transfer function from d.o.f. motions to the main gravitational channel
Expected cavity pole at 500 Hz
Requirements
Measurements (VSR1)
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Noise budget
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Linear noise projection
A feed-back loop can re-introduce noise (actuation or sensor noise) Linear noise projection is a well-known technique to measure the contribution of a feed-back loop
GW channel
error signal ITF TF
correction signal
Control
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Automatic measurement in Virgo
Noise budgets for longitudinal and angular controls are automated
Two examples from April 2008
Longitudinal control loops
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Angular control loops
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Other sources of noise / 1
Technical noises
Actuation noise (DAC and coil driver) Sensing noise (shot noise) Local oscillator phase noise Laser input power noise Laser frequency noise
Power noise (upper limit)
Frequency noise
Actuation noise (VSR1 estimate)
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Other sources of noise / 2
Environmental noise
Magnetic, seismic and acoustic coupling through clipping, diffused and scattered light, etc.
Typically non-linear
Deep modulation and large up-conversion
Difficult to identify and project
Impossible to measure environmental noise at the point of scattering Magnetic noise
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Other sources of noise / 2
Environmental noise
Magnetic, seismic and acoustic coupling through clipping, diffused and scattered light, etc.
Typically non-linear
Deep modulation and large up-conversion
Difficult to identify and project
Impossible to measure environmental noise at the point of scattering Dark fringe Seismometer
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Environmental noise projection
Main source of coupling: window at Brewster angle between main interferometer and detection tower
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Typical noise budget during VSR1
Control noise
Frequency noise Environmental noise Shot noise
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Typical NS-NS inspiral range during VSR1
Mpc
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Improvements after VSR1
Many improvements
Longitudinal and angular control noise reduction Actuator noise reduction Mitigation of diffused and scattered light problems Brewster window removal Calibration improvements …
NS-NS range [Mpc]
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Typical noise budget today
Eddy currents Actuation Environmental
Shot noise
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Non-stationary noise analysis
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Noise is non-stationary
Dark fringe noise (sensitivity) changes with time
Typical time constants from seconds to days
Need of a technique to monitor the non-stationarities Band-limited RMS (BRMS)
Integral of power in a limited frequency band
Typical dark fringe signal spectrum
BRMSi( t )
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Line identification algorithm
A narrow and large spectral line can dominate the BRMS in a band An algorithm has been developed to estimate the noise floor and identify lines
Useful also as a line identification tool
Very old data!
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BRMS monitoring during VSR1
An on-line process monitoring BRMS all over Virgo band-width BRMS is computed every second
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Typical non-stationarity
Noise is almost stationary on short time-scale (up to about 1 hour) Large noise floor variations over longer times
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Multi-dimensional linear regression / 1
The goal:
Correlate noise BRMS variation with slow changes in other interferometric signals Angular positions, powers, temperatures, residual RMS motions, etc…
The technique used is a multi-dimensional linear regression
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Multi-dimensional linear regression / 2
Each BRMS is a random variable, linear combination of auxiliary channels, plus some gaussian noise
BRMS in a given frequency band
Unknown coefficients
Auxiliary channels
Additive gaussian noise
Best estimate of coefficients is given by least square method (in matrix notation)
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Multi-dimensional linear regression / 3
The coefficients covariance matrix can be computed
Having an estimate of the noise variance
Finally confidence intervals on coefficients:
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Practical application
More than 100 auxiliary channels have been used for the analysis Downsampled to 10 mHz, using only Science Mode periods (excluded initial and final parts of each segment) Full linear regression computed Coefficients compatible with 0 within 3 are discarded Linear regression computed again with remaining channels
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Some results / 1
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Some results / 2
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Linear regression: conclusions
It is possible to reconstruct very well the slow noise nonstationarities It is also possible to select the most relevant auxiliary channels
Suspended benches position Micro-seismic conditions and alignment accuracy
After the end of the run, noise is much more stationary But no long enough periods of stable operations to repeat the analysis
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Glitches
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Fast noise variations
Dark fringe signal is affected by short (< 1s) periods of increased noise
Glitches
Need of a fast tool to track the largest one HACR = hierarchical algorithm for curves and ridges developed by the GEO600 group and implemented in Virgo
VirgoHACR
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HACR: principles
Compute short Fourier Transforms to obtain a timefrequency map
Simulated white noise + sine gaussian burst
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HACR: principles
Compute mean spectrum with a running time-average
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HACR: principles
Distance of each bin from mean, normalized with variance
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HACR: principles
Bins above high threshold generate a trigger Adjacent bins above lower threshold are clustered
One trigger
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HACR: principles
For each cluster several parameters are computed
Mean time and frequency Time and frequency width Total power Maximum and mean SNR …
During VSR1 HACR ran on-line, writing triggers to a database Allows easy storage and retrevial of trigger lists
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Dark fringe triggers
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Dark fringe triggers
Many classes distributed in different frequency regions Different origins identified
Frequency noise
Beam jitter
Power supplies
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Coincidence with auxiliary channels
Time-shift analysis: count time coincidence between two channels adding different time shifts Beam Monitoring System: steers the input beam
Before and after There are physical fixing BMS problem
coincidences
This signal could be used as a veto
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Conclusions
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Conclusions
Commissioning of the Virgo detector
Angular and (mainly) longitudinal control systems Other control system improvements
Noise studies
Measurement of control noise budget Estimation of frequency / power noise Collaboration with environmental noise group On-line data analysis tools NonStatMoni: BRMS monitor LineMonitor: line extraction and tracking VirgoHACR: glitch monitor Slow noise non-stationarity analysis
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Spare slides
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PSR 1916+13
Orbital period about 8 hours
E.M. waves
Gravitational waves
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VSR1 duty cycle
Duty Cycle Science Mode 81.4%
Longest Lock 94.3 h
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Laser lab benches
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Suspended benches
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DARM open loop transfer function
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PRCL open loop transfer function
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MICH open loop transfer function
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Noise subtraction
One auxiliary loop correction is filtered and added to DARM one TF computed from measurements to cancel the noise coupling
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Virgo sensitivity history
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Virgo-LSC detectors
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Coil drivers
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Suspended detection bench noise
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Faster noise non-stationarities
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