Output Feedback Attitude Tracking Control for a Rigid Spacecraft with Dynamic Uncertainty

被引：5
|
作者：
Xian Bin [1 ]
Huang Mu [1 ]
Li Dong [1 ]
Cui Cuijie [1 ]
Yang Kaiyan [1 ]
机构：
[1] Tianjin Univ, Sch Elect Engn & Automat, Tianjin 300072, Peoples R China
来源：
PROCEEDINGS OF THE 27TH CHINESE CONTROL CONFERENCE, VOL 2 | 2008年
关键词：
Spacecraft; Output feedback; Attitude control; Quaternion; uncertainty;
D O I：
10.1109/CHICC.2008.4605788
中图分类号：
TP [自动化技术、计算机技术];
学科分类号：
0812 ;
摘要：
In this paper, a nonlinear output feedback control mechanism is developed to address the attitude tracking problem of a rigid spacecraft system which contains uncertainty associated with dynamic model and is under the effect of external disturbance. The control strategy is based on limited assumption on the system dynamics. A set of filters are developed to compensate for the unmeasurable spacecraft's angular velocity. A semi-global asymptotic attitude tracking result is achieved while all the closed-loop states remain bounded.
引用
收藏
页码：464 / 468
页数：5
相关论文
共 50 条
  • [31] Attitude Tracking Control for Rigid Spacecraft with Arbitrary Convergence Time
    Xu, Yu-Tian
    Wu, Ai-Guo
    JOURNAL OF SYSTEMS SCIENCE & COMPLEXITY, 2024, 37 (06) : 2579 - 2594
  • [32] Attitude Tracking and Disturbance Rejection of Rigid Spacecraft by Adaptive Control
    Chen, Zhiyong
    Huang, Jie
    IEEE TRANSACTIONS ON AUTOMATIC CONTROL, 2009, 54 (03) : 600 - 605
  • [33] Fixed-time attitude tracking control for rigid spacecraft
    Zou, An-Min
    Kumar, Krishna Dev
    de Ruiter, Anton H. J.
    AUTOMATICA, 2020, 113
  • [34] Global adaptive stabilization using output feedback for spacecraft attitude tracking
    Miwa, H
    Akella, MR
    SPACEFLIGHT MECHANICS 2002, VOL 112, PTS I AND II, 2002, 112 : 345 - 357
  • [35] Attitude Sampling Tracking Control For A Rigid Spacecraft Via Backstepping
    Yang, Xiaoli
    Li, Jing
    Jia, Jinping
    Gao, Fei
    2019 9TH INTERNATIONAL CONFERENCE ON INFORMATION SCIENCE AND TECHNOLOGY (ICIST2019), 2019, : 92 - 96
  • [36] Predefined-Time Attitude Tracking Control of a Rigid Spacecraft
    Wang, Wencong
    Hou, Mingshan
    Liu, Bojun
    Qiao, Siyu
    Wu, Zhonghua
    2021 PROCEEDINGS OF THE 40TH CHINESE CONTROL CONFERENCE (CCC), 2021, : 427 - 432
  • [37] Adaptive Synergetic Optimal Control for Attitude Tracking of Rigid Spacecraft
    Ma Guangfu
    Huang Jing
    Liu Gang
    Li Chuanjiang
    2011 30TH CHINESE CONTROL CONFERENCE (CCC), 2011, : 1865 - 1870
  • [38] Fixed-time attitude tracking control for rigid spacecraft
    Wang, Zeng
    Su, Yuxin
    Zhang, Liyin
    IET CONTROL THEORY AND APPLICATIONS, 2020, 14 (05): : 790 - 799
  • [39] Adaptive output feedback tracking control of spacecraft formation
    Wong, H
    Kapila, V
    Sparks, AG
    INTERNATIONAL JOURNAL OF ROBUST AND NONLINEAR CONTROL, 2002, 12 (2-3) : 117 - 139
  • [40] Adaptive output feedback tracking control of multiple spacecraft
    Wong, H
    Kapila, V
    Spaxks, A
    PROCEEDINGS OF THE 2001 AMERICAN CONTROL CONFERENCE, VOLS 1-6, 2001, : 698 - 703
12345