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The structure design of small satellite full-physical simulation system
Xu ZG(徐志刚); Wang YJ(王亚军); He Y(贺云); Bai XL(白鑫林)
作者部门装备制造技术研究室
会议名称2015 IEEE International Conference on Cyber Technology in Automation, Control, and Intelligent Systems (CYBER)
会议日期June 8-12, 2015
会议地点Shenyang, China
会议录名称2015 IEEE International Conference on Cyber Technology in Automation, Control, and Intelligent Systems (CYBER)
出版者IEEE
出版地Piscataway, NJ, USA
2015
页码642-648
收录类别EI ; CPCI(ISTP)
EI收录号20161402187557
WOS记录号WOS:000380502300123
产权排序1
ISSN号2379-7711
ISBN号978-1-4799-8730-6
关键词Air-bearing Table Full-physical Simulation Disturbance Load Simulation Flexible Accessories
摘要The article presents a kind of small satellite disturbing loads full-physical simulation system which is used to deeply research and validate the control algorithms of orbit and attitude of small satellite under the effect of spacial disturbances. The system uses methods of air floating and hanging for gravity compensation of the five DOF air floating platform on which flexible solar wings have been installed. The main parts of the system have been designed and analyzed in the text. Finally, the feasibility of the system has been illustrated by the simulation that result from the combination of ANSYS and ADAMS softwares. The system proposed in this paper make it available that the satellite with flexible attachment as a whole be used for experiments under spacial disturbances on the ground, it is of great significance to suppress the vibration of flexible attachment and strengthen the stability of the position of satellite under spacial disturbances.
语种英语
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文献类型会议论文
条目标识符http://ir.sia.cn/handle/173321/17498
专题装备制造技术研究室
作者单位1.Equipment Manufacturing Technology Laboratory, Shenyang Institute of Automation (SIA), Shenyang, China
2.Department of Mechanical Engineering, Shenyang Ligong University, Shenyang, China
推荐引用方式
GB/T 7714
Xu ZG,Wang YJ,He Y,et al. The structure design of small satellite full-physical simulation system[C]. Piscataway, NJ, USA:IEEE,2015:642-648.
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