DocumentCode :
2850505
Title :
Gyroscope spin axis direction control for the Gravity Probe B satellite
Author :
Bencze, Willia J. ; Xiao, Yueming ; Hipkins, David N. ; Franklin, Gene F. ; Parkinson, Bradford W.
Author_Institution :
Dept. of Electr. Eng., Stanford Univ., CA, USA
Volume :
1
fYear :
1996
fDate :
11-13 Dec 1996
Firstpage :
480
Abstract :
Presented is a technique which can control the orientation of the spin axis of an electrostatically suspended vacuum gyroscope (ESVG) using residual torques generated by the rotor´s suspension system. A process of rotor shape “spin averaging” showed that the residual electrostatic torques take on a particularly simple form: they tend to cause the rotor to precess about the electrode axes. A time-optimal bang-bang control scheme was developed for the Gravity Probe B spacecraft which utilizes suspension voltages in the force null space to generate the torques which lead to controlled spin axis precessions. Laboratory tests confirm the spin averaged torque predictions
Keywords :
artificial satellites; attitude control; bang-bang control; electrostatic devices; general relativity; gravitation; gyroscopes; rotors; time optimal control; ESVG; controlled spin axis precessions; electrostatically suspended vacuum gyroscope; force null space; frame dragging; gravity probe B satellite; gyroscope spin axis direction control; relativity experiment; residual electrostatic torques; residual torques; rotor suspension system; spin axis orientation control; suspension voltages; time-optimal bang-bang control scheme; torque generation; Control systems; Electrostatics; Gravity; Gyroscopes; Probes; Rotors; Shape; Torque control; Vacuum systems; Vacuum technology;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Decision and Control, 1996., Proceedings of the 35th IEEE Conference on
Conference_Location :
Kobe
ISSN :
0191-2216
Print_ISBN :
0-7803-3590-2
Type :
conf
DOI :
10.1109/CDC.1996.574360
Filename :
574360
Link To Document :
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