In this paper, experimental verifications of various jerk-limited control designs are presented. The focus is on a large slew maneuver of a flexible spacecraft where the fast and accurate pointing is required at the end of the maneuver. Various control profiles are investigated including input shaping and jerk-limited optimal control profiles, especially to account the effect of jerk in the control profile. The control design is verified by the experiment using the Flexible Spacecraft Simulator (FSS).
Experiments on Jerk-Limited Slew Maneuvers of a Flexible Spacecraft
2006
21 pages
Report
No indication
English
AIAA-2006-6187 Experiments on Jerk-Limited Slew Maneuvers of a Flexible Spacecraft
British Library Conference Proceedings | 2006
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