Saturated Output Feedback Control for Global Asymptotic Attitude Tracking of Spacecraft

被引:9
|
作者
Xia, Yuquan [1 ]
Su, Yuxin [1 ]
机构
[1] Xidian Univ, Sch Electromech Engn, Xian 710071, Shaanxi, Peoples R China
关键词
ANGULAR VELOCITY-MEASUREMENT; CONTROL INPUT SATURATION; RIGID SPACECRAFT; CONTROL DESIGN; STABILIZATION; SYSTEMS; BODIES;
D O I
10.2514/1.G003566
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
[No abstract available]
引用
收藏
页码:2298 / +
页数:8
相关论文
共 50 条
  • [21] Finite-time output feedback attitude control of spacecraft
    Gao, Dai
    Lu, Jianting
    Wang, Benli
    [J]. Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica, 2012, 33 (11): : 2074 - 2081
  • [22] Output feedback control for spacecraft with coupled translation and attitude dynamics
    Pan, HZ
    Wong, H
    Kapila, V
    [J]. 2004 43RD IEEE CONFERENCE ON DECISION AND CONTROL (CDC), VOLS 1-5, 2004, : 4453 - 4458
  • [23] Output attitude tracking for flexible spacecraft
    Di Gennaro, S
    [J]. AUTOMATICA, 2002, 38 (10) : 1719 - 1726
  • [24] Distributed fixed-time output feedback attitude coordination tracking control for multiple rigid spacecraft
    Sui W.-S.
    Duan G.-R.
    Zhang M.-R.
    [J]. Kongzhi yu Juece/Control and Decision, 2021, 36 (05): : 1049 - 1058
  • [25] Velocity-free fixed-time output feedback attitude tracking control of rigid spacecraft
    Yin, Zheng
    Zou Zhanjie
    Wang, Yan
    Zhao, Bintao
    [J]. PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2023, 237 (07) : 1629 - 1636
  • [26] Fuzzy Adaptive Fault-Tolerant Output Feedback Attitude-Tracking Control of Rigid Spacecraft
    Huo, Baoyu
    Xia, Yuanqing
    Yin, Lijian
    Fu, Mengyin
    [J]. IEEE TRANSACTIONS ON SYSTEMS MAN CYBERNETICS-SYSTEMS, 2017, 47 (08): : 1898 - 1908
  • [27] Adaptive quaternion-based output feedback control for flexible spacecraft attitude tracking with input constraints
    Xiao, B.
    Hu, Q.
    Ma, G.
    [J]. PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART I-JOURNAL OF SYSTEMS AND CONTROL ENGINEERING, 2011, 225 (I2) : 226 - 240
  • [28] Comment on "Robust Saturated Finite Time Output Feedback Attitude Stabilization for Rigid Spacecraft"
    Su, Yuxin
    [J]. JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2017, 40 (06) : 1537 - 1537
  • [29] Robust H∞ output feedback control for attitude stabilization of a flexible spacecraft
    Wu, Shunan
    Wen, Shenghui
    [J]. NONLINEAR DYNAMICS, 2016, 84 (01) : 405 - 412
  • [30] Attitude cooperative control of spacecraft formation via output-feedback
    Lv, Yueyong
    Hu, Qinglei
    Ma, Guangfu
    Zhang, Jian
    [J]. AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, 2012, 84 (05): : 321 - 329