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Published byAmi Sullivan Modified over 9 years ago
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Deutsches SOFIA Institut Universität Stuttgart Second Gyro System for the SOFIA Telescope J.F. Wagner Deutsches SOFIA Institut, Universität Stuttgart, Germany
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Symposium Gyro Technology 20092 Deutsches SOFIA Institut Universität Stuttgart Wide Field Imager (WFI) Fine Field Imager (FFI) Focal Plane Imager (FPI) aircraft vibrations aero-acoustics controller commanded attitude actual attitude actuators structure and mechanics gyroscopes perturbations data fusion tracker correction Attitude Control: Inertial Stabilization + {
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Symposium Gyro Technology 20093 Deutsches SOFIA Institut Universität Stuttgart SOFIA’s Fiber Optic Gyroscopes Optical sensor module Opto-electronic module Initial situation Telescope pointing budget allocated for gyro drift: 0.04 arcsec Very low noise requirement dominated gyro design → Optical fiber length 3.4 km → Mean coil diameter150 mm → Closed loop operation Performance:Angular increment< 0.001 arcsec Dynamic range> 10.3 °/s Bandwidth> 1 kHz Random walk0.0003 °/√h In-run bias stability0.003 °/h
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Symposium Gyro Technology 20094 Deutsches SOFIA Institut Universität Stuttgart SOFIA’s Fiber Optic Gyroscopes
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Symposium Gyro Technology 20095 Deutsches SOFIA Institut Universität Stuttgart Constant Performance Two data sets available over a period of 9 years Data show very constant low noise behaviour Calibration 1999/2003 Calibration 2008
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Symposium Gyro Technology 20096 Deutsches SOFIA Institut Universität Stuttgart Spare part Repair Second Gyro System First possibility: Exchange of the gyro box Gyro Box 2 nd Gyro Box Nasmyth Tube ATCUTASCU Failure Gyro Box
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Symposium Gyro Technology 20097 Deutsches SOFIA Institut Universität Stuttgart Failure Second Gyro System Second possibility: Parallel system (hot standby) Gyro Box 2 nd Gyro Box Nasmyth Tube ATCUTASCU 2 nd ATCU Gyro BoxATCU
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Symposium Gyro Technology 20098 Deutsches SOFIA Institut Universität Stuttgart Second Gyro System Comparison: Advantages (+) / Disadvantages (–) / Neutral (0) Gyro Box Exchange Hot Standby Accuracy+– Cost–– Software modification0– ATCU failure– ++ “Save a mission”–++ Flexibility of schedule– +
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