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 ; Kapitel : 5 ; 105-137
16.09.2021
33 pages
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
Optimal Variable Amplitudes Input Shaping Control for Slew Maneuver of Flexible Spacecraft
Online Contents | 2017
|Optimal Variable Amplitudes Input Shaping Control for Slew Maneuver of Flexible Spacecraft
Online Contents | 2017
|Neural optimal control of flexible spacecraft slew maneuver
Online Contents | 2004
|