绳系系统轨道机动过程中的面内摆角抑制  

Librational Controller Design for a Tethered Satellite System during Orbital Maneuvering

作　　者：薛超[1] 谈树萍[1,2] 刘贺龙[1] 

机构地区：[1]北京控制工程研究所,北京100090 [2]空间智能控制技术国家级重点实验室,北京100190

出　　处：《空间控制技术与应用》2017年第2期21-27,共7页Aerospace Control and Application

基　　金：国家自然科学基金资助项目(61304037)

摘　　要：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.A controller is designed to restrain the in-plane libration of a tethered satellite system （TSS）. To stabilize the in-plane subsystem of TSS, a hierarchical iterative nonlinear sliding mode control is proposed. The stability of the closed-loop system is also proved. The validity of the proposed algorithm is demonstrated by numerical simulation results. Moreover, the advantages of the algorithm are presented via comparing with the traditional hierarchical sliding mode control.

关 键 词：绳系卫星系统 滑模控制 轨道机动 

分 类 号：V448[航空宇航科学与技术—飞行器设计]