This paper is concerned with the problem of slewing a large structure in space and suppressing any vibration at the same time. The structure is assumed to undergo large rigid-body motions and small elastic deformations. A perturbation method permits a maneuver strategy independent of the vibration control. Optimal control and pole placement techniques, formulated to include first-order actuator dynamics, are used to suppress the vibration during maneuver. The theory is illustrated by simultaneous maneuvering and vibration control of the Spacecraft Control Laboratory Experiment (SCOLE) model in a space environment.
Maneuvering and vibration control of flexible spacecraft
1987-09-01
Miscellaneous
No indication
English
Maneuvering and Vibration Control of Flexible Spacecraft
NTIS | 1987
|Maneuvering and vibration control of flexible spacecraft
NTRS | 1987
|Maneuvering of flexible spacecraft
AIAA | 1986
|Active vibration suppression for maneuvering spacecraft with high flexible appendages
Online Contents | 2017
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