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
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