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AN ANALYSIS MODEL TO PREDICT ROTATION ACCURACY OF HIGH-PRECISION SPINDLES CONSIDERING PART ERRORS AND DEFORMATION 会议论文
作者:  Sun, Yanhui;  Hong, Jun;  Guo, Junkang;  Zhang, Yanfei;  Wan, Shaoke
收藏  |  浏览/下载:4/0  |  提交时间:2019/11/19
Sensor-Based Inspection of the Formation Accuracy in Ultra-Precision Grinding (UPG) of Aspheric Surface Considering the Chatter Vibration 期刊论文
PHOTONIC SENSORS, 2018, 卷号: 8, 页码: 97-102
作者:  Lei, Yao;  Bai, Yue;  Xu, Zhijun
收藏  |  浏览/下载:8/0  |  提交时间:2019/11/21
Adaptive genetic algorithm-based method for antenna location optimization in RF relative measurement 会议论文
2018 NASA/ESA Conference on Adaptive Hardware and Systems, AHS 2018
作者:  Zijie, W.;  Rongke, L.;  Weiqing, M.;  Xiaoyan, S.;  Thompson, J.
收藏  |  浏览/下载:3/0  |  提交时间:2019/12/30
Sensor-Based Inspection of the Formation Accuracy in Ultra-Precision Grinding (UPG) of Aspheric Surface Considering the Chatter Vibration 期刊论文
Photonic Sensors, 2018, 卷号: 8, 期号: 2, 页码: 97-102
作者:  Lei, Y.;  Bai, Y.;  Xu, Z. J.
收藏  |  浏览/下载:4/0  |  提交时间:2019/09/17
Significantly Improved Protein Folding Thermodynamics Using a Dispersion-Corrected Water Model and a New Residue-Specific Force Field 期刊论文
JOURNAL OF PHYSICAL CHEMISTRY LETTERS, 2017
Wu, Hao-Nan; Jiang, Fan; Wu, Yun-Dong
收藏  |  浏览/下载:3/0  |  提交时间:2017/12/03
Adaptive control at launching using three loop autopilot (EI CONFERENCE) 会议论文
2011 2nd International Conference on Mechanic Automation and Control Engineering, MACE 2011, July 15, 2011 - July 17, 2011, Inner Mongolia, China
Zhang Y.
收藏  |  浏览/下载:18/0  |  提交时间:2013/03/25
In order to guarantee the precise initial flight trajectory  control the missile disturbance of large disturbance torque  three loop adaptive autopilot was researched. The characteristics of the projectile and three loop autopilot instruction formation characteristics were analysed. From equivalent pitching angle of lateral acceleration feedback loop  combined with the instruction of generalized error  autopilot structure was simplified  and three loop autopilot adaptive control law and stability were designed. The test data show that when disturbance torque was 600Nm  the attitude angle generalized error was -4.4. In the time lasted about 15s  late trajectory accuracy was within 1.0.Three loop autopilot adaptive control law was able to control the disturbance of initial trajectory and adapt to dynamic characteristics changes  control system stability. It was the initial trajectory accurate solution method of flight. 2011 IEEE.  


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