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Design and Analysis of Physical Simulation System for Satellite Rotating Panels
Yin M(尹猛); He Y(贺云); Xu ZG(徐志刚); Liu Z(刘哲); Shao XD(邵晓东)
作者部门装备制造技术研究室
会议名称2016 IEEE International Conference on Robotics and Biomimetics (ROBIO 2016)
会议日期December 3-7, 2016
会议地点Qingdao, China
会议录名称Proceedings of the 2016 IEEE International Conference on Robotics and Biomimetics (ROBIO 2016)
出版者IEEE
出版地New York
2016
页码2039-2044
收录类别EI ; CPCI(ISTP)
EI收录号20171403534761
WOS记录号WOS:000405724600342
产权排序1
ISBN号978-1-5090-4363-7
关键词Physical Simulation System Flexible Satellite Rotating Panels Structure Design Simulation Verification
摘要Flexible accessories is an important part of modern satellite, the elastic vibration is the main factor influencing the control performance of space vehicle, which make it necessary to test the performance of vibration suppression for the control system on the ground. The difficulty of physical simulation is to simulate the space microgravity environment, the length of solar array is large and frequency is low, which make it extremely difficult to build the space microgravity environment. In view of the above situation, this paper proposes a method of flexible solar simulator based on air flotation, and we design the physical simulation system based on equivalent spindle inertia and flexible frequency. Dynamic model is established for the simulation system to make sure that the system can equivalently simulate the torque characteristics of flexible satellite rotating panels, which reduces the difficulty to simulate ground microgravity environment. The rationality of the scheme is verified by the simulation results, whose results show that, the simulator has torque characteristics consistent with real solar panels, and we can achieve a smooth change of parameters by a simple operation to simulate different parameters and structure of the solar array. This method meets the test requirements and can effectively and efficiently examine the vibration performance of the control algorithm.
语种英语
引用统计
文献类型会议论文
条目标识符http://ir.sia.cn/handle/173321/19518
专题装备制造技术研究室
通讯作者Yin M(尹猛)
作者单位1.University of Chinese Academy of Sciences, Beijing CO, 100049, China
2.Shenyang Institute of Automation, Chinese Academy of Sciences, CO, 110179, China
3.College of Mechanical Engineering and Automation, Northeastern University, Shenyang, CO, 110819, China
4.College of Electrical Engineering, Shenyang University of Technology, CO, 110870, China
推荐引用方式
GB/T 7714
Yin M,He Y,Xu ZG,et al. Design and Analysis of Physical Simulation System for Satellite Rotating Panels[C]. New York:IEEE,2016:2039-2044.
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