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An improved magnetometer calibration and compensation method based on Levenberg-Marquardt algorithm for multi-rotor unmanned aerial vehicle 期刊论文
Measurement & Control, 2020, 卷号: 53, 期号: 3-4, 页码: 276-286
作者:  H. L. Wu,X. B. Pei,J. H. Li,H. B. Gao and Y. Bai
收藏  |  浏览/下载：2/0  |  提交时间：2021/07/06
Semi-active laser-guided energy transmission and simulation technology 期刊论文
Chinese Optics, 2019, 卷号: 12, 期号: 2, 页码: 256-264
作者:  K.-J.Liu;  X.-K.Miao;  C.-Y.Xu;  Y.Wang;  J.-Q.Zhang
收藏  |  浏览/下载：1/0  |  提交时间：2020/08/24
Gravity compensation optimization algorithm for large aperture spatial optical telescope 期刊论文
Guangxue Jingmi Gongcheng/Optics and Precision Engineering, 2018, 卷号: 26, 期号: 11, 页码: 2764-2775
作者:  He, Xu;  Yang, Xue;  Li, Yi;  Zhang, Xiao-Hui
收藏  |  浏览/下载：5/0  |  提交时间：2019/09/17
星载相机微振动下图像补偿技术研究 学位论文
博士: 中国科学院大学, 2015
作者:  许博谦
收藏  |  浏览/下载：40/0  |  提交时间：2015/11/30
无人机飞行控制系统若干关键技术研究 学位论文
博士: 中国科学院大学, 2014
段镇
收藏  |  浏览/下载：279/0  |  提交时间：2014/08/21
半捷联光电稳定平台误差分析与补偿研究 学位论文
博士: 中国科学院大学, 2014
赵明
收藏  |  浏览/下载：44/0  |  提交时间：2014/08/21
滚珠丝杠式电动舵机非线性分析及控制策略研究 学位论文
博士: 中国科学院大学, 2014
张明月
收藏  |  浏览/下载：196/0  |  提交时间：2014/08/21
Target filament accurate restoring system in high-energetic particle burst experiment 期刊论文
Guangxue Jingmi Gongcheng/Optics and Precision Engineering, 2014, 卷号: 22, 期号: 10, 页码: 2779-2786
Zhang Y.; Zhong X.; Xu Z.; Jin G.
收藏  |  浏览/下载：11/0  |  提交时间：2015/04/24
A design method for time sequential synchronization of semi-physical simulation on guidance weapon system 会议论文
2013 2nd International Conference on Mechatronics and Control Engineering, ICMCE 2013, August 28, 2013 - August 29, 2013, Dalian, China
Jiang R. K.; Li D. W.; Cui L. Z.
收藏  |  浏览/下载：12/0  |  提交时间：2014/05/15
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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