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空间碎片对绳系卫星冲击的影响分析
引用本文:刘丽丽,文浩,金栋平,胡海岩.空间碎片对绳系卫星冲击的影响分析[J].振动与冲击,2009,28(7):12-16.
作者姓名:刘丽丽  文浩  金栋平  胡海岩
作者单位:(南京航空航天大学振动工程研究所,飞行器结构力学与控制教育部重点实验室,南京 210016)
基金项目:国家自然科学基金(10672073和10372039)部分资助项目 
摘    要:摘 要:研究了绳系卫星受到太空碎片冲击时的最优控制响应。考虑系绳弹性和复杂边界约束,利用二阶微分包含及Legendre伪谱算法,提出了三维绳系卫星系统最优控制方法并给出了其回收过程最优控制的响应,获得了太空碎片对绳系卫星的冲击响应规律。


关 键 词:绳系卫星    最优控制    太空碎片    冲击  
收稿时间:2008-7-9
修稿时间:2008-8-8

Impact effects from space debris on a tethered satellite system
LIU Li-li,WEN Hao,JIN Dong-ping,HU Hai-yan.Impact effects from space debris on a tethered satellite system[J].Journal of Vibration and Shock,2009,28(7):12-16.
Authors:LIU Li-li  WEN Hao  JIN Dong-ping  HU Hai-yan
Affiliation:(Institute of Vibration Engineering Research, MOE Key Lab of Structure Mechanics and Control for Aircraft, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China)
Abstract:The optimal retrieval control for a three-dimensional tethered satellite system subject to different level of impacts from space debris was presented here. Tether elasticity and complex constraints were taken into consideration in the controller design firstly, which featured full exploitation of a second-order differential inclusion concept and a Legendre pseudo-spectral algorithm. The optimal tension and state profiles were solved with respect to the initial impact velocities. The various effects of impacts from space debris on the tethered satellite system were analyzed.
Keywords:tethered satellite system  optimal control  space debris  impact
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