Controller design and simulation of aircraft's automatic landing under complex atmospheric conditions

被引:0
|
作者
Zou, Xin-Sheng [1 ]
Li, Chun-Wen [1 ]
机构
[1] Department of Automation, Tsinghua University, Beijing 100084, China
关键词
D O I
暂无
中图分类号
学科分类号
摘要
引用
收藏
页码:1286 / 1288
相关论文
共 50 条
  • [21] Sliding-mode controller design of longitudinal automatic carrier landing system
    Guo Dong
    Lin Yan
    Proceedings of the 2007 Chinese Control and Decision Conference, 2007, : 195 - 198
  • [22] Design optimization of aircraft landing gear assembly under dynamic loading
    J. Wong
    L. Ryan
    I. Y. Kim
    Structural and Multidisciplinary Optimization, 2018, 57 : 1357 - 1375
  • [23] Design optimization of aircraft landing gear assembly under dynamic loading
    Wong, J.
    Ryan, L.
    Kim, I. Y.
    STRUCTURAL AND MULTIDISCIPLINARY OPTIMIZATION, 2018, 57 (03) : 1357 - 1375
  • [24] Adjustment method of automatic carrier landing system design criterion for scaled model aircraft
    Xu, Wangqiang
    Zhao, Rong
    Wang, Lixin
    PROCEEDINGS OF THE 36TH CHINESE CONTROL CONFERENCE (CCC 2017), 2017, : 6369 - 6375
  • [25] Simulation of large civil aircraft landing response under considerations of flexible airframe
    Nie, H. (hnie@nuaa.edu.cn), 1600, Nanjing University of Aeronautics an Astronautics (30):
  • [26] SIMULATION OF LARGE CIVIL AIRCRAFT LANDING RESPONSE UNDER CONSIDERATIONS OF FLEXIBLE AIRFRAME
    刘向尧
    聂宏
    魏小辉
    张明
    Transactions of Nanjing University of Aeronautics and Astronautics, 2013, (01) : 1 - 7
  • [27] Altitude controller design for vertical or short takeoff and landing aircraft with output rede finition method
    Zhu B.
    Chen Q.-W.
    Kongzhi Lilun Yu Yingyong/Control Theory and Applications, 2019, 36 (06): : 1009 - 1016
  • [28] Robust Adaptive Backstepping Controller Design for Aircraft Autonomous Short Landing in the Presence of Uncertain Aerodynamics
    Xin, Qi
    Shi, Zhongke
    JOURNAL OF AEROSPACE ENGINEERING, 2018, 31 (02)
  • [29] Design of Automatic Carrier-Landing Controller Based on Compensating States and Dynamic Inversion
    Wang, Lipeng
    Zhang, Zhi
    Zhu, Qidan
    Wen, Zixia
    IEEE ACCESS, 2019, 7 : 146939 - 146952
  • [30] Simulation system of integrative electronic display and automatic landing guidance for carrier-based aircraft
    Zhao, GR
    Liu, T
    Gao, QW
    System Simulation and Scientific Computing, Vols 1 and 2, Proceedings, 2005, : 1208 - 1212