本文主要研究内容
作者(2019)在《Research on Intelligent Control Technology in Helicopter Wind Tunnel Test》一文中研究指出:The helicopter wind tunnel test is a dynamic test with high speed, high difficulty and high risk. Traditional test methods often have some shortcomings, such as low efficiency, poor safety and labor i
Abstract
The helicopter wind tunnel test is a dynamic test with high speed, high difficulty and high risk. Traditional test methods often have some shortcomings, such as low efficiency, poor safety and labor i
论文参考文献
[1].Study about the Application of Numerical Wind tunnel to the Structure of Radar[A]. Mei qiyuan,Hu changming,Shen wenjun Nanjing Research Institute of Electronics Technology Mailbox of 1313-402,NanJing 210013,Jiangsu province,P.R. China.Proceedings of the Third Asia International Symposium on Mechatronics[C]. 2008[2].Back-Analysis of Mechanics Parameters of tunnel Based on Particle Swarm Optimization and Numerical Simulation[A]. JIANG Annan,Li Peng.Proceedings of 2011 International Conference on Advanced Materials and Computer Science(ICAMCS 2011 Part2)[C]. 2011[3].Study on the method of test and control system for low speed wind tunnel[A]. Yueming Yang,Kai Luo,Xingrong Bao,Yuankai Li.Proceedings of 2015 International Conference on Automation,Mechanical Control and Computational Engineering(AMCCE 2015)[C]. 2015[4].Situation Awareness Enhancement of Cockpit Synthetic Vision System: Visualization of Tunnel-in-the-Sky[A]. Huang Xuelin,Wang Jiangyun,Han liang,Ma Shidong School of Automation Science and Electrical Engineering,Beihang University Haidian District,100191 Beijing,China.Proceedings of 2009 9th International Conference on Electronic Measurement & Instruments(ICEMI’2009) Vol.3[C]. 2009[5].Low-speed wind tunnel testing control systems research[A]. J.B.Yao,Q.Y.Yang,Y.M.Yang.Proceedings of International Conference on Airworthiness & Fatigue-7th ICSAELS Series Conference[C]. 2013[6].Hypersonic aeroelastic response prediction using CFD/CSD approach[A]. Jinan Lyu,Li Guo,Zhanjun Chen,Ziqiang Liu.Abstract Book of the 7th International Conference on Fluid Mechanics[C]. 2015[7].Developing Dual-Surveillance and Dual-Tele-Paths in SCADA Networks of Tunnel/Mining Spaces[A]. HSU LiYen.2008(沈阳)国际安全科学与技术学术研讨会论文集[C]. 2008[8].Numerical simulation for fluid-structure interaction on the flutter behavior of membranes in a wind tunnel[A]. Zhen-hua Liu~(1,2),Qi-lin Zhang~1,Shao-xia Sun~2 (1.Department of Building Engineering,Tongji University,Shanghai 200092,China,(2.School of Civil Engineering,Shandong University,Jinan 250061,China).Proceedings of the 5th International Conference on Nonlinear Mechanics[C]. 2007[9].Experiment Investigation of Side Wall Boundary-Layer Blowing Control System of A Multi-element Airfoil Model in Wind Tunnel[A]. Zhang Lixiang~*,Xie Yajun National Key laboratory of science and technology on Aerodynamic Design and Research,NWPU,Xi’an 710072.The Proceedings of 2010 Asia-Pacific International Symposium on Aerospace Technology(Vol.1)[C]. 2010[10].IMC Based Temperature Control of Tunnel Kiln[A]. Yang Yinghua,Jiang Xin,Liu Chunrui,Qin Shukai College of Information Science and Engineering,Northeastern University,China No.3-11,Wenhua Road,Heping District,Shenyang,110004 China.Proceedings of the 8th International Conference on Measurement and Control of Granular Materials[C]. 2009
论文详细介绍
论文作者分别是来自第31届中国控制与决策会议的,发表于刊物第31届中国控制与决策会议2019-06-03论文,是一篇关于,第31届中国控制与决策会议2019-06-03论文的文章。本文可供学术参考使用,各位学者可以免费参考阅读下载,文章观点不代表本站观点,资料来自第31届中国控制与决策会议2019-06-03论文网站,若本站收录的文献无意侵犯了您的著作版权,请联系我们删除。
标签:第31届中国控制与决策会议2019-06-03论文;
:Research on Intelligent Control Technology in Helicopter Wind Tunnel Test论文
下载Doc文档