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Configuration maintaining control of three-body ring tethered system based on thrust compensation
文献类型:期刊
作者:Huang, Panfeng[1]  Liu, Binbin[2]  Zhang, Fan[3]  
机构:[1]Research Center for Intelligent Robotics, School of Astronautics, Northwestern Polytechnical University, Xi'an, China |National Key Laboratory of Aerospace Flight Dynamics, Northwestern Polytechnical University, Xi'an, China
[2]Research Center for Intelligent Robotics, School of Astronautics, Northwestern Polytechnical University, Xi'an, China |National Key Laboratory of Aerospace Flight Dynamics, Northwestern Polytechnical University, Xi'an, China
[3]Research Center for Intelligent Robotics, School of Astronautics, Northwestern Polytechnical University, Xi'an, China |National Key Laboratory of Aerospace Flight Dynamics, Northwestern Polytechnical University, Xi'an, China
通讯作者:Huang, PF (reprint author), Northwestern Polytech Univ, Sch Astronaut, Res Ctr Intelligent Robot, Xian 710072, Peoples R China.; Huang, PF (reprint author), Northwestern Polytech Univ, Natl Key Lab Aerosp Flight Dynam, Xian 710072, Peoples R China.
年:2016
期刊名称:ACTA ASTRONAUTICA影响因子和分区
卷:123
页码范围:37-50
增刊:正刊
学科:工程学
收录情况:SCI(E)(WOS:000384626700005)  EI(20161102108099)  
所属部门:航天学院
被引频次:8
人气指数:809
浏览次数:801
基金:National Natural Science Foundation of China [11272256, 61005062, 60805034]
关键词:Space remote observation; Three-body ring tethered system; Spinning dynamics; Configuration maintaining control
摘要:
Space multi-tethered systems have shown broad prospects in remote observation missions. This paper mainly focuses on the dynamics 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, and then validate the suitability of this model by numerical simulation. Subsequently, LP (Likins-Pringle) i ...More
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