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Configuration maintaining control of three-body ring tethered system based on thrust compensation
文献类型:会议
作者:Huang, Panfeng[1]  Lu, Zhenyu[2]  Liu, Binbin[3]  Zhang, Fan[4]  Meng, Zhongjie[5]  Liu, Zhengxiong[6]  
机构:[1]Research Center of Intelligent Robotics, National Key Laboratory of Aerospace Flight Dynamics, School of Astronautics, Northwestern Polytechnic University, Xian, Shanxi Province, China
[2]Research Center of Intelligent Robotics, National Key Laboratory of Aerospace Flight Dynamics, School of Astronautics, Northwestern Polytechnic University, Xian, Shanxi Province, China
[3]Research Center of Intelligent Robotics, National Key Laboratory of Aerospace Flight Dynamics, School of Astronautics, Northwestern Polytechnic University, Xian, Shanxi Province, China
[4]Research Center of Intelligent Robotics, National Key Laboratory of Aerospace Flight Dynamics, School of Astronautics, Northwestern Polytechnic University, Xian, Shanxi Province, China
[5]Research Center of Intelligent Robotics, National Key Laboratory of Aerospace Flight Dynamics, School of Astronautics, Northwestern Polytechnic University, Xian, Shanxi Province, China
[6]Research Center of Intelligent Robotics, National Key Laboratory of Aerospace Flight Dynamics, School of Astronautics, Northwestern Polytechnic University, Xian, Shanxi Province, China
年:2015
通讯作者:Huang, Panfeng(pfhuang@nwpu.edu.cn)
会议名称:2015 IEEE International Conference on Information and Automation, ICIA 2015 - In conjunction with 2015 IEEE International Conference on Automation and Logistics
页码范围:2275-2280
会议地点:Yunnan, China
会议开始日期:2015-09-28
会议结束日期:2015-08-10
收录情况:EI(20161102092917)  
所属部门:航天学院
人气指数:1265
浏览次数:1253
语言:外文
摘要:
Space multi-tethered systems have shown broad prospects in remote observation missions. This paper mainly focuses on the dynamics modeling and configuration maintaining control of space spinning three-body ring tethered system for such mission. Firstly, we establish the spinning dynamic model of the three-body ring tethered system considering the elasticity of the tether using Newton-Euler method. Subsequently, a control strategy based on thrust compensation, namely thrust to simulate tether com ...More
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