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A vibration modulation method for natural mode measurement of external-cavity diode laser 期刊论文
AIP ADVANCES, 2018, 卷号: 8
作者:  Quan, Wei;  Liu, Sizhe;  Zhai, Yueyang
收藏  |  浏览/下载:10/0  |  提交时间:2019/12/30
A dual closed-loop drive and control system of photoelastic modulator for atomic magnetometer 期刊论文
MEASUREMENT SCIENCE AND TECHNOLOGY, 2018, 卷号: 29
作者:  Quan, Wei;  Wang, Qinghua;  Zhai, Yueyang
收藏  |  浏览/下载:2/0  |  提交时间:2019/12/30
A composite anti-disturbance control scheme for attitude stabilization and vibration suppression of flexible spacecrafts 期刊论文
JOURNAL OF VIBRATION AND CONTROL, 2017, 卷号: 23, 页码: 2470-2477
作者:  Wang, Zhen;  Wu, Zhong;  Li, Lijun;  Yuan, Jun
收藏  |  浏览/下载:7/0  |  提交时间:2019/12/30
采用光学成像法的航空稳定平台振动幅度检测 期刊论文
2016, 2016
王书民; 张爱武; 胡少兴; 孟宪刚; 段乙好; 孙卫东; WANG Shumin; ZHANG Aiwu; HU Shaoxing; MENG Xiangang; DUAN Yihao; SUN Weidong
收藏  |  浏览/下载:4/0
Monocular line tracking for the reduction of vibration induced during image acquisition 期刊论文
JOURNAL OF VIBROENGINEERING, 2015, 卷号: 17, 期号: [db:dc_citation_issue], 页码: 655-661
作者:  Afolabi, David;  Man, Ka Lok;  Liang, Hai-Ning;  Guan, Sheng-Uei;  Krilavicius, Tomas
收藏  |  浏览/下载:8/0  |  提交时间:2019/12/02
REAL-TIME VIBRATION REDUCTION IN UAV'S IMAGE SENSORS USING EFFICIENT HOUGH TRANSFORM 会议论文
作者:  Afolabi, David;  Shen, Zhun;  Krilavicius, Tomas;  Hahanov, Vladimir;  Litvinova, Eugenia
收藏  |  浏览/下载:11/0  |  提交时间:2019/12/03
Design of stable image platform on airborne camera (EI CONFERENCE) 会议论文
2011 International Conference on Advanced Design and Manufacturing Engineering, ADME 2011, September 16, 2011 - September 18, 2011, Guangzhou, China
Qian Y.; Yang L.; Hu F.; Hong X.
收藏  |  浏览/下载:11/0  |  提交时间:2013/03/25
Modulation transfer function resulting from random vibration was analyzed. To conclude that the effect of angular displacement was the major factor. Allowable MTF degradation was represented  and 34dB reduction was achieved at frequency of 100HZ. With the help of MSC.ADAMS simulation software  and convert allowable MTF degradation into stable system design parameters  simulated curve proves correct for isolator  which can guide perfect design for stabilization system. Based on the spatial mechanism and translational principle of parallelogram  and the irrotational displacement mechanism was tested by optical method  an irrotational displacement isolator was developed. It can meet the requirements of irrotational displacement and damp. An instance was given  coupled angle is less than 8?  it can satisfy the demand of aerial imaging. (2011) Trans Tech Publications.  
Dynamic coupling analysis and modeling for stabilized platform of rolling-pitching seeker (EI CONFERENCE) 会议论文
2011 International Conference on Electric Information and Control Engineering, ICEICE 2011, April 15, 2011 - April 17, 2011, Wuhan, China
Ai X.; Liu H.; Jiang Z.; Jia H.
收藏  |  浏览/下载:9/0  |  提交时间:2013/03/25
Missile's attitude change will be delivered to visual axis through stabilized platform during maneuvering flight  and the missile vibration will be an interference source to visual axis stabilization. In order to solve this problem  the coupling relationship between missile attitude and visual axis is obtained by Coordinate transformation. When the seeker stably tracks a target  the angular velocity of visual axis in inertial space is zero  so the relative angular velocity of roll axis and pitch axis can be derived for servo control. According to Oura dynamics equation  the dynamic models of roll axis and pitch axis were established and kinetic equations of two axises were obtained. The dynamic models can provide theoretical basis to developing research of servo control system and structural optimization design of stabilized platform. Finally  some measures could reduce the dynamic coupling between the framework was given. 2011 IEEE.  
基于二次稳定算法的结构主动控制仿真分析 期刊论文
2010, 2010
张微敬; 闫维明; 钱稼茹; ZHANG Wei-jing; YAN Wei-ming; QIAN Jia-ru
收藏  |  浏览/下载:1/0
Simulation study of active control based on quadratic stabilization algorithm 期刊论文
2010, 2010
Zhang Wei-jing; Yan Wei-ming; Qian Jia-ru
收藏  |  浏览/下载:3/0


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