Recursive dynamic modeling for attitude control of fully flexible spacecraft with central body and appendages
Jianyao Wang,
Hongdong Wang
Abstract:A spacecraft composed of a central body and flexible appendages is a typical rigid-flexible coupling system. Current modeling methods generally regard the central body as rigid. As the central body becomes larger and more flexible, the elastic deformation of the central body may not be ignored. In this study, considering the flexibility effect of the central body and based on the recursive kinematics, a complete coupled dynamic model of the orbit, attitude, and elastic deformation of a fully flexible spacecraf… Show more
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