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Advanced LIGO UK 1 LIGO-G040064-00-K OSEM Development UK Advanced LIGO project Stuart Aston University of Birmingham for the UK Advanced LIGO Team LSC.

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Presentation on theme: "Advanced LIGO UK 1 LIGO-G040064-00-K OSEM Development UK Advanced LIGO project Stuart Aston University of Birmingham for the UK Advanced LIGO Team LSC."— Presentation transcript:

1 Advanced LIGO UK 1 LIGO-G040064-00-K OSEM Development UK Advanced LIGO project Stuart Aston University of Birmingham for the UK Advanced LIGO Team LSC Livingston, March 2004 LIGO-G040064-00-K

2 Advanced LIGO UK 2 LIGO-G040064-00-K Overview Requirements: –Generic OSEM Requirements –OSEM Noise Performance Requirements OSEM Development Concepts: –Geometric based OSEMs –Interferometer based OSEM –Performance Summary Conclusions: –OSEM Recommendations UK Advanced LIGO Team

3 Advanced LIGO UK 3 LIGO-G040064-00-K Generic OSEM Requirements Range: –3mm (peak-peak) working range (1.06mm rms), incorporating:  1mm operating range  ½mm tolerance for relative positioning of OSEM and sensed mass Fit: (sensors must fit actuator) –Sense motion of mass through bore hole of coil former –Constraints (for the case of the TM quad) restrict layout envelope to 40mm (diameter) x 70mm (length), including connectors and mounts Vacuum Compatibility: –Sensor components must meet the vacuum compatibility requirements appropriate to an Advanced LIGO vacuum chamber Electrical Compatibility: –Sensor drive and output must be compatible with the specification of cables passing through the SEI system (ideally using LIGO cables) UK Advanced LIGO Team

4 Advanced LIGO UK 4 LIGO-G040064-00-K OSEM Noise Performance Requirements Sensitivity Requirements for Local Control OSEMs: –Assume Eddy current damping and ISC feedback, most stringent requirement is MC longitudinal = 1.72x10 -11 m/  Hz * –For more detail, see E040108-00-K Sensitivity Requirements for Global Control OSEMs: –Science mode noise requirement about 10Hz:  1x10 -10 m/  Hz * –This figure also encompasses: Transverse horizontal sensors on all suspensions Other, less critical, degrees of freedom on RM and MC –Note that almost half the OSEMs fit one or other of these categories * Figures extracted from “Recommendation of a design for the OSEM sensors” document LIGO-E040108-00-K UK Advanced LIGO Team

5 Advanced LIGO UK 5 LIGO-G040064-00-K OSEM Concept Development Geometric Sensors: –Prototype developed by C.C. Speake and S.M. Aston at the University of Birmingham –Parallel independent development undertaken by our collaborator N.A. Lockerbie at the University of Strathclyde Basic Operation: –Use a reasonably collimated and strongly modulated light source –High power IRLED (880nm) emitter (OP-50L) –Beam passes through optical system which is partly mounted on an extension of the sensed mass –Beam is incident on a split photodiode detector –Detected photocurrents are demodulated to produce sum and difference signals: Difference output provides useful displacement measurement read-out Sum signal enables active intensity stabilisation of emitter output UK Advanced LIGO Team

6 Advanced LIGO UK 6 LIGO-G040064-00-K Geometric Sensor Prototype (University of Birmingham): OSEM Concept Development UK Advanced LIGO Team Translation (± x) Photodiode IRLED OD-50L Cylindrical Lens Translation (± y) Rotation (  z ) 10mm41mm (25mm)

7 Advanced LIGO UK 7 LIGO-G040064-00-K Geometric Sensor Prototype (University of Strathclyde): OSEM Concept Development UK Advanced LIGO Team (of OD-50L) (BPW34S)

8 Advanced LIGO UK 8 LIGO-G040064-00-K OSEM Concept Development Interferometric Sensor: –Development by C. Speake and S. Aston at the University of Birmingham Basic Operation: –Use a collimated laser diode light source –Low power (3mW) emitter (HL6314MG) at 635nm –3 output interferometer has single element “bug-eye” pd’s at each output –Polarising beam-splitter gives quadrature outputs for 2 ports –3 rd port output is 180 0 out of phase (allows subtraction of dc offsets) –3 outputs are subtracted in pairs (via 2 difference amplifiers) resulting in 2 dc corrected channels to be read-out –Signal processing allows the fringes to be counted as well as fractional fringe measurements to be made –Dynamic range limited by the coherence length of the laser diode UK Advanced LIGO Team

9 Advanced LIGO UK 9 LIGO-G040064-00-K Interferometric Sensor Prototype (University of Birmingham): OSEM Concept Development UK Advanced LIGO Team PD2 QWP LD HWP BS QWP PBS PD3 PD1 Laser Diode and Collimation Optics Adjustable Mirror Suspension Mirror Cat’s Eye Attenuator and aperture Polariser Quarter-wave plateNon-polarising beam-splitter 70mm Polarising beam-splitterHalf-wave plate Mirror A BC D E FG Pd2Pd1Pd3 40mm

10 Advanced LIGO UK 10 LIGO-G040064-00-K OSEM Development Performance Geometric Sensors: –Shot noise limited performance of  1.5x10 -11 m/  Hz about 10Hz and essentially flat down to 1Hz. –But this result was not achievable over the whole working range! –Common suspect component of excess noise is the IRLED emitter –Significant risk that there are no other alternative high power, low noise and good beam quality devices available Interferometric Sensor: –Performance of  5x10 -13 m/  Hz about 10Hz is achievable without a high power source or any modulation scheme –Perceived risk in complexity of construction and laser diode noise performance and MTBF (device screening maybe required) UK Advanced LIGO Team

11 Advanced LIGO UK 11 LIGO-G040064-00-K Conclusions OSEM Recommendations: –We recommend the use of the interferometric design wherever high sensitivity is required together with basic (modified) initial LIGO OSEMs for global control and certain other locations Summary of Rationale: –Interferometric concept is the most secure approach to reaching the sensitivity requirement –Higher component cost partly offset by possible elimination of eddy current dampers UK Advanced LIGO Team


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