北京航空航天大学主页平台系统乐挺--乐挺--论文

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乐挺 ( 副教授 ) 赞
的个人主页 http://shi.buaa.edu.cn/yueting/zh_CN/index.htm
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[1] .T. Yue, X. Zuo, L. Wang, J. Geng and H. Zhang, "Similarity Relations of PID Flight Control Parameters of Scaled-Model and Full-Size Aircraft," in IEEE Transactions on Aerospace and Electronic Systems, vol. 58, no. 4, pp. 2950-2960, Aug. 2022, doi: 10.1109/TAES.2022.3143481.
[2] .Lixin WANG, Ning ZHANG, Hailiang LIU, Ting YUE, Stability characteristics and airworthiness requirements of blended wing body aircraft with podded engines, Chinese Journal of Aeronautics, Volume 35, Issue 6, 2022, Pages 77-86.
[3] .Wang, L. , Yin, H. , Guo, Y. , Yue, T. , & Jia, X. .. Closed-loop motion characteristic requirements of receiver aircraft for probe and drogue aerial refueling[J]. Aerospace science and technology, 2019, 93(Oct.):105293.1-105293.10.
[4] .Yue T, Xu Z, Wang L, Wang T. Sliding mode control design for oblique wing aircraft in wing skewing process. Chinese Journal of Aeronautics, 2019; 32(2):263-271.
[5] .Yue T, Zhang X, Wang L, Ai J. Flight dynamic modeling and control for a telescopic wing morphing aircraft via asymmetric wing morphing. Aerospace Science and Technology, 2017; 70:328-38.
[6] .Wang L, Xu Z, Yue T* . Dynamic characteristics analysis and flight control design for oblique wing aircraft. Chinese Journal of Aeronautics, 2016; 29(6):1664-72.
[7] .Yue T, Wang L, Ai J. Gain self-scheduled H∞ control for morphing aircraft in the wing transition process based on an LPV model. Chinese Journal of Aeronautics, 2013; 26(4):909-17.
[8] .Yue T, Wang L, Ai J. Longitudinal linear parameter varying modeling and simulation of morphing aircraft. Journal of Aircraft, 2013; 50(6): 1673-81.
[9] .Yue T, Wang L, Ai J. Longitudinal multibody dynamic characteristics of Z-wing morphing aircraft. Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica 2010; 31(4):679-86. (被评为2010-2014年《航空学报》高被引频次论文，全国共22篇)

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