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CORC

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Design and verification of high-precision multi-star simulator with a wide field of view 期刊论文
Chinese Optics, 2020, 卷号: 13, 期号: 6, 页码: 1343-1351
作者:  H.-G. Xu,B. Han,M.-L. Li,H.-T. Ma,P.-Y. Zhang and D.-H. Ju
收藏  |  浏览/下载：2/0  |  提交时间：2021/07/06
A feasibility study of dynamic verification for tumor target delineation and dose delivery using a six degrees of freedom motion phantom 期刊论文
INTERNATIONAL JOURNAL OF RADIATION RESEARCH, 2018, 卷号: 16, 期号: 4, 页码: 411-420
作者:  Xu, G.;  Xiong, Z.;  Wang, H.;  Jiang, H.;  Li, B.
收藏  |  浏览/下载：63/0  |  提交时间：2020/05/21
Design of optical system for sun sensor with birefringence in uniaxial crystal 会议论文
Changsha, China, May 21, 2018 - May 23, 2018
作者:  Li, Yanli;  Gao, Dong;  Pan, Deng
收藏  |  浏览/下载：34/0  |  提交时间：2019/01/31
Attitude Calculation Method Based on CPF-EKF for Large Load Plant Protection UAV 期刊论文
Nongye Jixie Xuebao/Transactions of the Chinese Society for Agricultural Machinery, 2018, 卷号: 49, 期号: 6, 页码: 24-31 and 77
作者:  Wu, Helong;  Bai, Yue;  Pei, Xinbiao;  Ma, Ping;  Peng, Cheng
收藏  |  浏览/下载：18/0  |  提交时间：2019/09/17
High accuracy three-dimensional attitude angle measuring device 期刊论文
guangxue jingmi gongcheng/optics and precision engineering, 2016, 卷号: 24, 期号: 5, 页码: 963-970
作者:  Sun, Guo-Yan;  Gao, Li-Min;  Bai, Jian-Ming;  Yang, Dong-Lai;  Pan, Liang
收藏  |  浏览/下载：20/0  |  提交时间：2016/10/13
Structure design of nanometer positioning stage with a large stroke 期刊论文
Guangxue Jingmi Gongcheng/Optics and Precision Engineering, 2016, 卷号: 24, 期号: 5
作者:  Chen, Q.
收藏  |  浏览/下载：9/0  |  提交时间：2017/09/11
机载全光纤相干多普勒激光测风雷达 学位论文
博士: 中国科学院上海光学精密机械研究所, 2015
作者:  刁伟峰
收藏  |  浏览/下载：201/0  |  提交时间：2016/11/28
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：48/0  |  提交时间：2014/08/21
Body inertial-sensing network platform for wearable 3D gesture analysis 会议论文
2nd International Symposium on Bioelectronics and Bioinformatics, ISBB 2011, Suzhou, China
作者:  Yan-Wei Guo;  Wei-Zhong Wang;  Guan-Zheng Liu;  Guo-Ru Zhao;  Bang-Yu Huang
收藏  |  浏览/下载：16/0  |  提交时间：2015/08/25
Control method research on wide flight envelope aerocraft (EI CONFERENCE) 会议论文
2nd Annual Conference on Electrical and Control Engineering, ICECE 2011, September 16, 2011 - September 18, 2011, Yichang, China
Duan Z.
收藏  |  浏览/下载：19/0  |  提交时间：2013/03/25
The flying qualities of aerocraft was directly effected by the autopilot  for the wide flight envelope aerocraft  on the basic of analyzing the typical trajectory  the three loop autopilots of roll stability  pitch and yaw were designed  using single-mode Transient suppression method  the overload due to control surface transition deflection was avoided when control parameters changing  the verification was done by non-linear simulation. The result showed that: Under the action of the disturbance torque  the maximum roll was less than 5  the range of the aerocraft was from 13.5km to 22.4km  the max height was about 5100m  the max deviation of lateral was about 42m  the maximum elevator deflection was less than 6.5 the control law was applicable within the effective range. An autopilot design method of wide flight envelope aerocraft was provided. 2011 IEEE.  

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