Attitude control of a large flexible spacecraft using three-axis mass expulsion control
Guidance and Control Conference ; 1973 ; Key Biscayne , FL , U.S.A.
1973-01-01
Conference paper
Electronic Resource
English
Optimal attitude control for three-axis stabilized flexible spacecraft
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|Flexible Spacecraft Three Axis Attitude Maneuver by Active Vibration Control
DOAJ | 2009
|Adaptive mass expulsion attitude control system
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|Attitude Control of Large Flexible Spacecraft
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