For further improving the performances of attitude control methods, vibration controllers for flexible appendages have been introduced and the coupling control method has been developed. The basic idea of the coupling control method is to combine the attitude stabilization theory with a vibration controller. The attitude of the platform and elastic vibrations of flexible appendages are controlled simultaneously.
Rigid-Flexible Coupling Control Method for Flexible Spacecraft
Rigid-Flexible Coupling Dynamics and Control of Flexible Spacecraft with Time-Varying Parameters ; Kapitel : 6 ; 139-170
16.09.2021
32 pages
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
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