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) | |
2015 | |
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 |
关键词 | Air-bearing table Full-physical simulation Disturbance Load simulation Flexible Accessories |
页码 | 642-648 |
中文摘要 | 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. |
收录类别 | EI ; CPCI(ISTP) |
产权排序 | 1 |
会议录 | 2015 IEEE International Conference on Cyber Technology in Automation, Control, and Intelligent Systems (CYBER) |
会议录出版者 | IEEE |
会议录出版地 | Piscataway, NJ, USA |
语种 | 英语 |
ISSN号 | 2379-7711 |
ISBN号 | 978-1-4799-8730-6 |
WOS记录号 | WOS:000380502300123 |
内容类型 | 会议论文 |
源URL | [http://ir.sia.cn/handle/173321/17498] |
专题 | 沈阳自动化研究所_装备制造技术研究室 |
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]. 见:2015 IEEE International Conference on Cyber Technology in Automation, Control, and Intelligent Systems (CYBER). Shenyang, China. June 8-12, 2015. |
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