Abstract
A rigid - flexible coupling dynamic model is established for full reflection of the coupling between deformation of flexible body and large angle maneuver. Considering uncertainties of the flexible spacecraft a traditional PD controller and an adaptive attitude adjustment controller are designed to solve the attitude adjustment problem of the rigid-flexible coupling spacecraft based on Lyapunov method. These two controllers are compared in simulation analyses; results show that compared with the traditional PD controller, the adaptive controller can effectively suppress the influence of disturbance torques, with higher precision and better robustness, and be able to fulfill the important demand of attitude adjustment for the rigid-flexible coupling spacecraft.
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Yan, X., Dong, Y., Zhengxian, Y., Zhaowei, S. (2015). Research on Attitude Adjustment Control for Large Angle Maneuver of Rigid-Flexible Coupling Spacecraft. In: Liu, H., Kubota, N., Zhu, X., Dillmann, R., Zhou, D. (eds) Intelligent Robotics and Applications. ICIRA 2015. Lecture Notes in Computer Science(), vol 9244. Springer, Cham. https://doi.org/10.1007/978-3-319-22879-2_3
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DOI: https://doi.org/10.1007/978-3-319-22879-2_3
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