H∞ feedback for attitude control of liquid-filled spacecraft (vol 24, pg 46, 2001)

被引：0
|
作者：
Kuang, JL [1 ]
Leung, AYT [1 ]
机构：
[1] Univ Manchester, Manchester M13 9PL, Lancs, England
来源：
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS | 2001年 / 24卷 / 05期
关键词：
D O I：
10.2514/2.4820
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
引用
收藏
页码：1053 / 1053
页数：1
相关论文
共 50 条
  • [41] Fault-tolerant attitude control for liquid-filled flexible spacecraft without angular velocity measurements based on disturbance observer
    Song, Xiaojuan
    Li, Xuesong
    Lu, Shufeng
    Song, Xiaowen
    JVC/Journal of Vibration and Control, 2024, 30 (5-6): : 1143 - 1158
  • [42] Fault-tolerant attitude control for liquid-filled flexible spacecraft without angular velocity measurements based on disturbance observer
    Song, Xiaojuan
    Li, Xuesong
    Lu, Shufeng
    Song, Xiaowen
    JOURNAL OF VIBRATION AND CONTROL, 2024, 30 (5-6) : 1143 - 1158
  • [43] Dynamics and Control of Mass-Variable Liquid-Filled Spacecraft With Combined Nonlinear Slosh
    Liu, Feng
    Yue, Baozeng
    Ma, Bole
    IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, 2024, 60 (03) : 3509 - 3522
  • [44] Using Sliding Mode Control Method to Suppress Fuel Sloshing of a Liquid-Filled Spacecraft
    Shi XingYu
    Qi RuiYun
    2015 27TH CHINESE CONTROL AND DECISION CONFERENCE (CCDC), 2015, : 1268 - 1273
  • [45] Vegetable oils for liquid-filled transformers (vol 18, pg 6, 2002)
    Oommen, TV
    IEEE ELECTRICAL INSULATION MAGAZINE, 2002, 18 (02) : 5 - 5
  • [46] Attitude dynamics and control of spacecraft with a partially filled liquid tank and flexible panels
    Liu, Feng
    Yue, Baozeng
    Zhao, Liangyu
    ACTA ASTRONAUTICA, 2018, 143 : 327 - 336
  • [47] ATTITUDE DYNAMICS AND CONTROL OF LIQUID FILLED SPACECRAFT WITH LARGE AMPLITUDE FUEL SLOSH
    Deng, M. -L.
    Yue, B. -Z.
    JOURNAL OF MECHANICS, 2017, 33 (01) : 125 - 136
  • [48] Disturbance Separation-Based Antidisturbance Attitude Control for Flexible Liquid-Filled Spacecrafts
    Zhu, Baopeng
    Tcng, Hao
    Meng, Yan
    Zhu, Yukai
    2024 3RD CONFERENCE ON FULLY ACTUATED SYSTEM THEORY AND APPLICATIONS, FASTA 2024, 2024, : 1480 - 1485
  • [49] Robust H∞ output feedback control for attitude stabilization of a flexible spacecraft
    Wu, Shunan
    Wen, Shenghui
    NONLINEAR DYNAMICS, 2016, 84 (01) : 405 - 412
  • [50] Magnetic attitude control of bias momentum spacecraft by bounded linear feedback (vol 70, pg 419, 2017)
    Luo, Weiwei
    Zhou, Bin
    AEROSPACE SCIENCE AND TECHNOLOGY, 2018, 75 : 386 - 387
12345