Spacecraft Attitude Stabilization Using Optimal Sliding Mode Control

摘要：

The attitude stabilization problem for a spacecraft is addressed through the combination of optimal control and sliding mode variable structure control method. We first determine an optimal sliding manifold for the kinematical subsystem of the spacecraft. Then a variable structure controller, which is based on equivalent control and the optimal sliding surface, is designed for the whole dynamical and kinematical system. An important feature of the methodology is that when the sliding manifold is reached, the attitude variables will be stabilized to the origin in the sense of optimality with respect to a quadratic cost functional. The proposed controller is also robust to external disturbances. Simulations are performed to demonstrate the effectiveness of the proposed optimal sliding mode controller.

作者: Chuanjiang Li Yibo Wang Liang Xu Zhongzhao Zhang

作者单位: Control Science and Engineering Department,Harbin Institute of Technology,Harbin,150001,China Research Center on Communications,Harbin Institute of Technology,Harbin,150001,China

会议类型: 国际会议

会议名称: The 3rd International Symposium on Systems and Control in Aeronautics and Astronautics(第三届航空航天系统与控制国际会议 ISSCAA 2010)

会议地点: 哈尔滨

会议语种:英文

页码: 1095-1099

在线出版日期: 2010-01-08（万方平台首次上网日期，不代表论文的发表时间）