In Chapter 5, an optimization method for variable amplitude input shaping attitude maneuver was proposed. And in Chapter 6, a coupled control method of attitude control and flexible structure vibration control was proposed for attitude tracking of flexible spacecraft with time-varying parameters
Rigid-Flexible Coupling Control Experiments
Rigid-Flexible Coupling Dynamics and Control of Flexible Spacecraft with Time-Varying Parameters ; Chapter : 7 ; 171-184
2021-09-16
14 pages
Article/Chapter (Book)
Electronic Resource
English
Rigid-Flexible Coupling Control Method for Flexible Spacecraft
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