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Phase camera development for gravitational wave detectors

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Presentation on theme: "Phase camera development for gravitational wave detectors"— Presentation transcript:

1 Phase camera development for gravitational wave detectors
Kazuhiro Agatsuma Martin van Beuzekom, David Rabeling, Guido Visser, Hans Verkooijen, Wilco Vink, Jo van den Brand 4th/June/2014 TIPP at Amsterdam 2014/June/4

2 Contents Phase camera is prepared for Advanced VIRGO Background
Gravitational waves GW detector VIRGO Marginally stable power recycling cavity Phase camera Principle Setup plan in AdV Prototype experiment at Nikhef Selection of components Summary and plan 2014/June/4

3 Gravitational waves Predicted by A. Einstein (1916)
Nobody detect it directly yet Indirect evidence Hulse and Taylor pulsar (1974) => Nobel prize (1993) BICEP2 (2014 in discussion) Direct observations will make a new method to observe universe Binary neutron star Black hole Super nova Inflation Unknown source etc… General relativity Beginning of universe Gravitational waves y z x 2014/June/4

4 Gravitational wave detector
Michelson Interferometer y Fabry-Perot Michelson Interferometer Power recycled Fabry-Perot Michelson Interferometer x Dual recycled Fabry-Perot Michelson Interferometer Power recycling mirror Laser EOM BS Fabry-Perot Cavity fp Signal recycling mirror Input Mode Cleaner Output Mode Cleaner Modulation-Demodulation (Pound–Drever–Hall technique) is used to operate IFO (control position and angle) Photo detector 2014/June/4

5 VIRGO Nikhef contributes to VIRGO
(Collaboration between France, Italy, Netherlands, Poland and Hungary) Upgrade VIRGO => advanced VIRGO (AdV) (Italy, Pisa) [ Worldwide competition to the first detection LIGO (USA) KAGRA (Japan) After the first detection World competition => World corroboration 2014/June/4

6 Marginally stable recycling cavity
VIRGO uses marginally stable recycling cavity Degeneration of higher order modes (HOMs) (Sideband power reduction can easily happen by aberration of mirrors) Control becomes unstable Aberrations Thermal lens Substrate inhomogeneities Surface shape errors ITM CO2 laser Wave front sensor PRM ITM BS Pick-off Solution: Thermal Compensation System (TCS) Sensor: Phase camera, Actuator: CO2 laser with compensation plate 2014/June/4

7 Phase Camera Frequency selective wave front sensor
Heterodyne detection Pin-hole scanning IFO (Pick-off mirror in IFO) PM for IFO EOM Test beam (with PM: fp) fp BS AOM Demodulation fH, fH+fp, fH-fp Reference beam (Frequency shift by fH) fH I Scanner Q Pin-hole Mapping of amplitude and phase 2014/June/4

8 Setup plan in AdV Phase camera will be placed on three ports
PC1: Input beam [f1 - f5] PC2: Power recycling cavity [f1, f4] PC3: Output beam [f2] PC1 CO2 laser PC2 EOM IMC PC3 : Arm cavity control (common) : SRC : PRC : Support for f1 : Input MC OMC Five sidebands will be used 2014/June/4

9 Setup plan in AdV Frequency shifter: Fiber coupled AOM
PC1: Input beam (Injection bench) PC2: Power recycling cavity (B4) PC3: Output beam (B1p) 2014/June/4

10 Prototype test at Nikhef
- Current setup - Test beam: Phase modulator (EOM): DC -> 250 MHz Reference beam: Frequency shift (AOM): 80 MHz Scanner: Galvanometer (GVS012) Photo-detector : New focus 1811 (125 MHz) DSP: LAPP fast ADC/FPGA board (400MHz Clock) AdV Real-time system signal processing Each sideband is selective 2014/June/4

11 Prototype test at Nikhef
Laser EOM AOM Galvanometer PD 2014/June/4

12 Mapping result (preliminary)
Carrier Test beam: 10MHz PM Power ratio (test beam and reference beam) is not optimized here => Calculation of SNR using actual parameters is in progress The phase between carrier and sidebands should be identical in the ideal IFO => Subtraction of those shows aberration map! Test Reference USB 2014/June/4

13 Scanning pattern (Archimedes' spiral)
32 x 32 pixels: 16 Hz 128 x 128 pixels: 64 Hz 256 x 256 pixels: 128 Hz In the case of the total acquisition time of 1 second to make one pattern (According to a simulation, a total acquisition time of at least 2-5 s [0.03 s] is necessary in order to keep sufficient precision of the phase measurement) Standard aperture diameter: 5 mm Test beam size: w = (2.5) / 3 = 833 um Quickest acquisition is 0.25 s (128 x 128 pixels, 256 Hz) with our scanner (Requirement: 100 x 100 pixels) 2014/June/4

14 Scanner (PZT scanner) ~300 Hz 5 mm PD 20 cm Tilt angle range:
50 mrad (±25 mrad) to scan 5 mm range, a half a maximum voltage is necessary with 20 cm distance The quickest operation is 300 Hz 2014/June/4

15 Photodiode board New PD has been developed at Nikhef (close to completion) Flat response up to 700MHz FCI-InGaAs-55 Active area diameter = 55 mm (pin-hole) NEP 2.66e-15 W/rtHz Flat window, AR coated DC output and RF TIA: HITTITE 799LP3E 10 kOhm DC – 700MHz 46 nV/rtHz output noise (spec) = 4.6 pA/rtHz input referrred Shot noise limited if Idiode > ~66 uA (VIR-0439A-13) 2014/June/4

16 Digital demodulation board
ADC fh fh +/- f1..f5 Hann* cosine LUT 16k sine PD in atan I Q Df 11x ‘DFT-slice’ cntr 0..N-1 sample clock power to DAQ block f1..f5 Digital Demodulation at 11 (fixed) frequencies (fh+/f1..f5) in parallel 14 bit ADC at 500 MS/s + Xilinx Virtex-7 FPGA Measure phase (and power) using 16k samples per ‘pixel’ can measure 32 k ‘pixels’ per second, frequency resolution ~30 kHz Best resolution when using external ref. frequencies (i.e. diff. phase measurement) s = ~0.3 mRad at 211 MHz (VIR-0439A-13) 2014/June/4

17 Optical layout design (PC1)
z=0 (※) preliminary design Optical layout is in progress 2014/June/4

18 Summary and Plan Summary
Phase camera can observe wave fronts for each PM sideband => Useful monitor for TCS in Virgo Prototype experiment is on going Component selection has done High speed PD and digital board are being prepared at Nikhef Plan (in progress) SNR calculation using actual parameters Optical layout drawings 2014/June/4


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