During the attitude maneuver of the flexible spacecraft, the attitude movement of the spacecraft body will excite the elastic vibration of the flexible attachment [1–3]. In return, the vibration would induce attitude oscillation after maneuver, which will downgrade the performance of payloads in spacecraft.
Optimal Variable Amplitudes Input Shaping Control for Slew Maneuver of Flexible Spacecraft
Rigid-Flexible Coupling Dynamics and Control of Flexible Spacecraft with Time-Varying Parameters ; Chapter : 5 ; 105-137
2021-09-16
33 pages
Article/Chapter (Book)
Electronic Resource
English
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