【摘 要】
：
The attitude maneuver control of a spacecraft with large flexible solar arrays is studied in this paper.The main objective is to apply classical control methodology to achieve high-precision attitude
【机 构】
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School of Aeronautics and Astronautics, Dalian University of Technology
【出 处】
：
The 4th International Conference on Dynamics, Vibration and
论文部分内容阅读
The attitude maneuver control of a spacecraft with large flexible solar arrays is studied in this paper.The main objective is to apply classical control methodology to achieve high-precision attitude maneuver.The dynamics and kinematics of a large flexible spacecraft are firstly proposed.A classical PID control law is then designed to stabilize spacecraft central rigid body.
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