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
01.01.1990
Aufsatz (Konferenz)
Keine Angabe
Englisch
Decentralized slew maneuver control of large flexible spacecrafts
Tema Archiv | 1990
|Design issues in the control of large flexible spacecraft slew maneuvers
Tema Archiv | 1990
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