Finite-time attitude regulation control for a rigid spacecraft under input saturation

被引：0
|
作者：
Du, Haibo [1 ]
Cheng, Yingying [1 ]
Lie, Yigang [1 ]
机构：
[1] Hefei Univ Technol, Sch Elect Engn & Automat, Hefei 230009, Peoples R China
来源：
2014 11TH WORLD CONGRESS ON INTELLIGENT CONTROL AND AUTOMATION (WCICA) | 2014年
基金：
中国博士后科学基金;
关键词：
attitude control; finite-time control; input saturation; STABILIZATION; TRACKING; SYSTEMS; STABILITY;
D O I：
暂无
中图分类号：
TP [自动化技术、计算机技术];
学科分类号：
0812 ;
摘要：
The problem of attitude regulation for a rigid spacecraft under input saturation is studied in this paper. Based on the technique of finite-time control and the model structural features, a novel finite-time attitude controller is proposed. The bound of a proposed finite-time controller can be adjusted to any small level to accommodate the actuation bound in practical implementation. A simulation example is given to demonstrate the efficiency of the proposed method.
引用
收藏
页码：1647 / 1651
页数：5
相关论文
共 50 条
  • [1] Finite-time attitude stabilization of rigid spacecraft under input saturation
    Cheng, Ying-Ying
    Du, Hai-Bo
    He, Yi-Gang
    [J]. Kongzhi yu Juece/Control and Decision, 2015, 30 (08): : 1386 - 1392
  • [2] Finite-time output feedback attitude control for rigid spacecraft under control input saturation
    Zou, An-Mm
    de Ruiter, Anton H. J.
    Kumar, Krishna Dev
    [J]. JOURNAL OF THE FRANKLIN INSTITUTE-ENGINEERING AND APPLIED MATHEMATICS, 2016, 353 (17): : 4442 - 4470
  • [3] Disturbance observer based finite-time attitude control for rigid spacecraft under input saturation
    Hu, Qinglei
    Li, Bo
    Qi, Juntong
    [J]. AEROSPACE SCIENCE AND TECHNOLOGY, 2014, 39 : 13 - 21
  • [4] Robust Finite-Time Spacecraft Attitude Control under Input Saturation
    Tan Xiao
    Hu Qinglei
    [J]. PROCEEDINGS OF THE 35TH CHINESE CONTROL CONFERENCE 2016, 2016, : 10673 - 10678
  • [5] Finite-time spacecraft attitude control under input magnitude and rate saturation
    An-Min Zou
    Krishna Dev Kumar
    Anton H. J. de Ruiter
    [J]. Nonlinear Dynamics, 2020, 99 : 2201 - 2217
  • [6] Adaptive Finite-Time Control for Attitude Tracking of Spacecraft under Input Saturation
    Guo, Yong
    Huang, Bing
    Wang, Shuo
    Li, Ai-jun
    Wang, Chang-qing
    [J]. JOURNAL OF AEROSPACE ENGINEERING, 2018, 31 (02)
  • [7] Finite-time spacecraft attitude control under input magnitude and rate saturation
    Zou, An-Min
    Kumar, Krishna Dev
    de Ruiter, Anton H. J.
    [J]. NONLINEAR DYNAMICS, 2020, 99 (03) : 2201 - 2217
  • [8] Robust Finite-time Attitude Tracking Control of Rigid Spacecraft Under Actuator Saturation
    Chen, Hai-Tao
    Song, Shen-Min
    Zhu, Zhi-Bin
    [J]. INTERNATIONAL JOURNAL OF CONTROL AUTOMATION AND SYSTEMS, 2018, 16 (01) : 1 - 15
  • [9] Robust Finite-time Attitude Tracking Control of Rigid Spacecraft Under Actuator Saturation
    Hai-Tao Chen
    Shen-Min Song
    Zhi-Bin Zhu
    [J]. International Journal of Control, Automation and Systems, 2018, 16 : 1 - 15
  • [10] Finite-Time Coordinated Attitude Control for Spacecraft Formation Flying Under Input Saturation
    Hu, Qinglei
    Zhang, Jian
    Friswell, Michael I.
    [J]. JOURNAL OF DYNAMIC SYSTEMS MEASUREMENT AND CONTROL-TRANSACTIONS OF THE ASME, 2015, 137 (06):
12345