基于有限元模型的飞行器柔性附件分散化滑模控制

研究分散化滑模控制在大型柔性附件振动控制领域中的应用。在设计控制系统时，滑模控制滑模面通过最小化最优价值函数得到，控制器采用饱和控制器。受控系统受到任意不可测量和不确定性外部扰动以及初始位移。分别利用分散化控制和集中控制方法对结构进行控制，仿真结果表明，当具有初始位移或受到不确定性外扰时，分散化控制非常有效。最后研究表明分散化控制方法所求解的Riccati方程数量远远少于集中控制方法，特别是大系统。

Decentralized Sliding Mode Control for a Spacecraft Flexible Appendage Based on Finite Element Method

This paper is devoted to study the application of the decentralized sliding mode control method, which is used to reduce the vibration of large spacecraft flexible appendage. In the process of control design, the sliding surface of sliding mode control is determined by minimizing the optimal cost function, and the controller is the saturation controller. The controlled structure is subject to arbitrary, unmeasurable and uncertainty disturbance forces and initial displacement. The decentralized control method and the centralized control method are used to control vibration of the structure respectively. When the system is subjected to the initial displacement or external disturbance, the computer simulation shows that both of these control methods perform effectively, but the number of Riccati equation of the decentralized method is far smaller than that of centralized control method, especially in a large system.