挠性空间飞行器的双回路控制器设计  

A DOUBLE LOOPS CONTROLLER DESIGNMETHOD FOR LARGE FLEXIBLE SPACECRAFT

作　　者：刘春梅[1] 沈毅[1] 胡恒章[1] 

机构地区：[1]哈尔滨工业大学控制工程系

出　　处：《空间科学学报》1999年第2期181-186,共6页Chinese Journal of Space Science

摘　　要：针对大型挠性空间结构频率低、阻尼小，刚体与各挠性模态之间互相耦合等特点，提出了一种双回路控制器的设计方法．回路的设计采用了最优滑动模态的变结构设计方法．且考虑了鲁棒稳定性问题．最后，给出了结果的数字仿真，从仿真曲线可以看出，对于基于模态截断的大型挠性空间飞行器,该设计方法具有一定的鲁棒性．In this paper, a double loops controller design method is provided in accordancewith the characteristics of large flexible spacecraft, such as low frequency, low damping and coupling between rigid body and flexible appendages. Optimal sliding-modecontrol method is used, and robust stability is considered. Finallyg numerical simulations show that vibration suppression and accurate pointing are accomplishedby using two separate control loops with certain robust property. Based on modetruncation modle of the flexible spacecraft.

关 键 词：双回路控制器 变结构 挠性 空间飞行器 

分 类 号：V448.2[航空宇航科学与技术—飞行器设计]