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Micro-vibration test of a reaction wheel after the mechanical test and transferring property through a shafting 会议论文
Hefei, China, 2018-11-26
作者:  Cui, Kai;  She, Wenji;  Gao, Xiong;  Li, Zhiguo;  Zheng, Zhiqi
收藏  |  浏览/下载：58/0  |  提交时间：2019/07/01
Angular micro-vibration test of an agile satellite high resolution camera based on liner accelerometer 会议论文
Xi'an, China, 2018-12-05
作者:  Cui, Kai;  Zheng, Zhiqi;  Gao, Xiong;  Yang, Yongqing;  Li, Zhiguo
收藏  |  浏览/下载：44/0  |  提交时间：2019/04/02
Robust Finite-time Observer Design for Rigid Spacecraft with Reaction Wheel Friction 会议论文
35th Chinese Control Conference (CCC), Chengdu, PEOPLES R CHINA, 2016-07-27
作者:  Niu Guanglin;  Hu Qinglei
收藏  |  浏览/下载：5/0  |  提交时间：2019/12/30
Robust Finite-time Observer Design for Rigid Spacecraft with Reaction Wheel Friction 会议论文
PROCEEDINGS OF THE 35TH CHINESE CONTROL CONFERENCE 2016, 2016-01-01
作者:  Niu Guanglin;  Hu Qinglei
收藏  |  浏览/下载：5/0  |  提交时间：2019/12/30
Sliding Mode Observer based Composite Controller for Spacecraft Attitude Control System with Reaction Wheel Friction 会议论文
2015 34TH CHINESE CONTROL CONFERENCE (CCC), 2015-01-01
作者:  Zhang Peixi;  Qiao Jianzhong;  Zhang Yabin;  Guo Lei;  Wang Sen
收藏  |  浏览/下载：2/0  |  提交时间：2020/01/06
Design and Analysis of a Two-Axis-Magnetic Bearing with Permanent Magnet Bias for Magnetically Suspended Reaction Wheel 会议论文
7th International Conference on Intelligent Systems and Knowledge Engineering, ISKE 2012, Beijing, China, 2012-12-15
作者:  Han, Bangcheng;  Zheng, Shiqiang;  Li, Haitao
收藏  |  浏览/下载：2/0  |  提交时间：2020/01/06
Observer-based robust sliding mode control for spacecraft attitude maneuver subject to reaction wheel friction 会议论文
64th International Astronautical Congress 2013, IAC 2013, Beijing, 2013-09-23
作者:  Wu S.;  Wu Z.;  Wu G.
收藏  |  浏览/下载：1/0  |  提交时间：2019/12/13
Parameter identification of reaction wheel disturbance model based WLS-SVR method 会议论文
4th International Conference on Information Technology for Manufacturing Systems, ITMS 2013, Auckland, New zealand, 2013-08-28
作者:  Wang, Yun Feng;  Cheng, Wei;  Xia, Ming Yi;  Wu, Shuang
收藏  |  浏览/下载：2/0  |  提交时间：2020/01/06
Design of semi-physical simulation for small satellite by virtual display (EI CONFERENCE) 会议论文
2011 3rd International Conference on Mechanical and Electronics Engineering, ICMEE 2011, September 23, 2011 - September 25, 2011, Hefei, China
Xu K.; Lv Y.; Jin G.
收藏  |  浏览/下载：19/0  |  提交时间：2013/03/25
Semi-physical simulation of attitude control system is the more synthetically test and verify for designing of small satellite control system. It is an important means of small satellite development. However  the results of current semi-physical simulation system have a lot of non-intuitive. Compare with the actual environment  the simulation environment still has striking disparity. So the shortcomings affect precision of simulation. Based on the virtual display technology  the group semi-physical simulation system has been constructed for attitude control of small satellite due to the combination with xPC real-time environment  the simulation computer  high-precision single-axis air-bearing turntable  reaction wheel  air thrust device  fiber gyroscopes  sensors synchronizer  power subsystem and wireless devices virtual display computer etc. Semi-physical simulation achieved the visual simulation in orbit and tracked new information of virtual environment of space into real-time simulation computer. Simulation results show that the simulation system for real-time attitude and orbit position of small satellite semi-physical simulation has an excellent display effect. At the same time  Real-time transfuse of orbit information provides a more accurate space environment simulation. The simulation system of small satellite attitude control to design and evaluate the more direct and convenient. (2012) Trans Tech Publications  Switzerland.  

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