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针对绳系卫星系统轨道机动过程中面内摆角抑制问题进行控制器设计.仅考虑面内摆角子系统下,针对绳系系统的动力学模型,提出了分层迭代非线性滑模控制方法.证明控制方法设计的控制律使系统所有状态渐近稳定.通过数学仿真验证方法的有效性和优势.
Aiming at the in-plane swing angle restraint in orbital maneuvering of a satellite system, the controller is designed. Considering only the in-plane swing angle sub-system, a layered iterative nonlinear sliding mode control method is proposed for the dynamic model of a rope system. It is proved that the control law of the control method design is asymptotically stable for all states of the system, and the validity and advantage of the method are verified through mathematical simulation.