Robust integrated flight/propulsion control design for a STOL aircraft

被引：0
|
作者：
Wang, Tao
Meng, Qingming
机构：
来源：
Hangkong Dongli Xuebao/Journal of Aerospace Power | 1999年 / 14卷 / 04期
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：437 / 439
相关论文
共 50 条
  • [21] INTEGRATED FLIGHT PROPULSION CONTROL-SYSTEM CONSIDERATIONS FOR FUTURE AIRCRAFT APPLICATION
    VIZZINI, RW
    MECHANICAL ENGINEERING, 1984, 106 (07) : 90 - 90
  • [22] Integrated Flight Control Design for a Large Flexible Aircraft
    Theis, Julian
    Pfifer, Harald
    Balas, Gary
    Werner, Herbert
    2015 AMERICAN CONTROL CONFERENCE (ACC), 2015, : 3830 - 3835
  • [23] PROPULSION SYSTEMS FOR SUPERSONIC V/STOL AIRCRAFT
    LEWIS, WJ
    JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME, 1990, 112 (02): : 206 - 211
  • [24] Control allocation for a V/STOL aircraft based on robust fuzzy control
    FAN Yong
    Science China(Information Sciences), 2011, 54 (06) : 1321 - 1326
  • [25] Control allocation for a V/STOL aircraft based on robust fuzzy control
    Yong Fan
    XianYu Meng
    XiLi Yang
    Kai Liu
    JiHong Zhu
    Science China Information Sciences, 2011, 54 : 1321 - 1326
  • [26] Robust control of transition maneuvers for a class of V/STOL aircraft
    Naldi, Roberto
    Marconi, Lorenzo
    AUTOMATICA, 2013, 49 (06) : 1693 - 1704
  • [27] Control allocation for a V/STOL aircraft based on robust fuzzy control
    Fan Yong
    Meng XianYu
    Yang XiLi
    Liu Kai
    Zhu JiHong
    SCIENCE CHINA-INFORMATION SCIENCES, 2011, 54 (06) : 1321 - 1326
  • [28] A ROBUST MODEL REFERENCE ADAPTIVE CONTROL FRAMEWORK FOR INTEGRATED FLIGHT PROPULSION SYSTEM
    Wang, Haonan
    Wang, Xi
    PROCEEDINGS OF THE ASME TURBO EXPO: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, VOL 5, PT I, 2020,
  • [29] INTEGRATED FLIGHT/PROPULSION CONTROL FOR HELICOPTERS
    ROCK, SM
    NEIGHBORS, K
    JOURNAL OF THE AMERICAN HELICOPTER SOCIETY, 1994, 39 (03) : 34 - 42
  • [30] LOW-SPEED TURNING FLIGHT PATH CONTROL OF A STOL AIRCRAFT
    KANNO, S
    KAMIMURA, M
    OHTA, H
    CHUBACHI, T
    TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, 1995, 38 (119) : 16 - 37
12345