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CORC

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The aircraft autopilot design of parameters changing in a wide range (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
Zhen D.; Yue Z.
收藏  |  浏览/下载：20/0  |  提交时间：2013/03/25
Autopilot is an important part of aircraft  Under the action of the disturbance torque  for the flight parameters of aircraft Changing in a wide range  the range was about 16km  on the basic of analyzing the typical trajectory  the max height was about 5100m  the trajectory of feature points were selected  the deviation of lateral was about 12m  taking pitch control loop for example  the maximum angle of attack was about 3.6  a sub- PID autopilot was designed using classical control theory  the maximum elevator deflection was less than 5  using single-mode Transient suppression method  the maximum aileron deflection was less than 2  the overload due to control surface transition deflection was avoided when control parameters changing  the maximum roll was less than 5  the verification was done by non-linear simulation. The result showed that: the phase margin of autopilot was greater than 30  the response of overload can accurately track the given overload instruction. An autopilot design method of aircraft of parameter changes in a wide range was provided. 2011 IEEE.  the bandwidth was more than 14rad / s  the settling time was less than 0.7s  the maximum overshoot was 23.3%  
ELECTERA - A Step towards the Development of a Techno Economic Risk Analysis Scheme for future Electric Aircraft 会议论文
ISABE, 2011
Georgios Doulgeris; Huw Edwards; Amir S. Gohardani; Riti Singh
收藏  |  浏览/下载：17/0  |  提交时间：2013/09/18
More Electric Engine Architecture for Aircraft Engine Application 会议论文
ASME, Vancouver, British Columbia, Canada, 2011-06-06
Noriko Morioka; Hitoshi Oyori; Daiki Kakiuchi; Kanji Ozawa
收藏  |  浏览/下载：12/0  |  提交时间：2012/07/13
Simulation of arcing fault in aircraft wiring system 会议论文
2011 1st International Conference on Electric Power Equipment - Switching Technology, ICEPE2011, Xi'an, 2011-10-23
作者:  Wang Y.;  Dong E.;  Cheng F.;  Huang Y.;  Zou J.
收藏  |  浏览/下载：3/0  |  提交时间：2019/12/18
Application of computer vision in performance test of aircraft engine nozzle 期刊论文
2011 International Conference on Electric Information and Control Engineering, ICEICE 2011 - Proceedings, 2011, 页码: 1186-1189
作者:  Huang, Xiaofeng;  Long, Yonghong
收藏  |  浏览/下载：1/0  |  提交时间：2020/01/05
Research on modulation strategy for two-stage matrix converter in more electric aircraft 期刊论文
Diangong Jishu Xuebao/Transactions of China Electrotechnical Society, 2011, 卷号: 26, 页码: 8-14
作者:  Xiao, Kun;  Wang, Lina;  Pei, Xiaoyu
收藏  |  浏览/下载：1/0  |  提交时间：2020/01/06
Failure detection for control surface of aircraft based on electric actuator 会议论文
2nd International Conference on Intelligent Control and Information Processing, ICICIP 2011, Harbin, China, 2011-07-25
作者:  Xiong, Xiao;  Zhang, Ping;  Zhang, Peng
收藏  |  浏览/下载：1/0  |  提交时间：2020/01/06
Research on Energy Transmission Capacity Improvement of the Aircraft Electric Power System 期刊论文
JOURNAL OF AIRCRAFT, 2011, 卷号: 48, 页码: 456-461
作者:  Lv, Hong;  Zhao, Jia
收藏  |  浏览/下载：1/0  |  提交时间：2020/01/06
Design of stability augmentor for aircraft nose wheel steering system based on Hopfield network identification algorithm 会议论文
2011 International Conference on Electric Information and Control Engineering, ICEICE 2011, Wuhan, China, 2011-04-15
作者:  Zhu, Dan-Dan;  Jia, Yu-Hong
收藏  |  浏览/下载：1/0  |  提交时间：2020/01/06
Modeling and analysis of concrete-filled steel structure under aircraft impact 会议论文
Washington, DC, United states, August 28, 2011 - August 31, 2011
作者:  Huo, Jin;  Hu, Zirong;  Sun, Yuping
收藏  |  浏览/下载：13/0  |  提交时间：2020/11/15

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