The dynamics and control of arbitrary slew maneuvers of a large flexible spacecraft are developed. The dynamics of slew maneuvers are nonlinear and include the coupling between the rigid orbiter and the flexible appendage. A decentralized control scheme is used to perform a large-angle slew maneuver about an arbitrary axis in space and to suppress the vibrations of the flexible appendage during and after the maneuver.
Slew maneuvers of large flexible spacecrafts
1990-01-01
Conference paper
No indication
English
Decentralized slew maneuver control of large flexible spacecrafts
Tema Archive | 1990
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