Sliding mode attitude tracking of rigid spacecraft with disturbances

被引：141
|
作者：
Lu, Kunfeng [1 ]
Xia, Yuanqing [1 ]
Zhu, Zheng [1 ]
Basin, Michael V. [2 ]
机构：
[1] Beijing Inst Technol, Sch Automat, Beijing 100081, Peoples R China
[2] Autonomous Univ Nuevo Leon, Dept Phys & Math Sci, San Nicolas De Los Garza, Nuevo Leon, Mexico
来源：
JOURNAL OF THE FRANKLIN INSTITUTE-ENGINEERING AND APPLIED MATHEMATICS | 2012年 / 349卷 / 02期
基金：
中国国家自然科学基金;
关键词：
VARIABLE-STRUCTURE CONTROL; FLEXIBLE SPACECRAFT; NONLINEAR-SYSTEMS; ROBUST-CONTROL; STABILIZATION; REJECTION; CONTROLLER; GUIDANCE;
D O I：
10.1016/j.jfranklin.2011.07.019
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 attitude tracking control problem of a spacecraft nonlinear model with external disturbances and inertia uncertainties is addressed in this paper. First, a new sliding mode controller is designed to ensure the asymptotic convergence of the attitude and angular velocity tracking errors against external disturbances and inertia uncertainties by using a modified differentiator to estimate the total disturbances. Second, an adaptive algorithm is applied to compensating the disturbances, by which another sliding mode controller is successfully designed to achieve a high performance on the attitude tracking in the presence of the inertia uncertainties, external disturbances and actuator saturations. Finally, simulation results are presented to illustrate effectiveness of the control strategies. (c) 2011 The Franklin Institute. Published by Elsevier Ltd. All rights reserved.
引用
收藏
页码：413 / 440
页数：28
相关论文
共 50 条
  • [41] Rigid spacecraft attitude control using adaptive integral second order sliding mode
    Tiwari, Pyare Mohan
    Janardhanan, S.
    Nabi, Mashuq Un
    AEROSPACE SCIENCE AND TECHNOLOGY, 2015, 42 : 50 - 57
  • [42] Distributed Adaptive Full Order Sliding Mode Control for Attitude Synchronization of Rigid Spacecraft
    Meng, Huan
    Song, Zhuoyue
    Latifu, Nsubuga
    Yan, Kai
    Wu, Qinghe
    Liu, Xiangdong
    2019 IEEE 15TH INTERNATIONAL CONFERENCE ON CONTROL AND AUTOMATION (ICCA), 2019, : 887 - 892
  • [43] Attitude Tracking of Rigid Spacecraft With Bounded Input
    Wang Xibin
    Guo Shuli
    Han Lina
    2017 4TH INTERNATIONAL CONFERENCE ON INFORMATION SCIENCE AND CONTROL ENGINEERING (ICISCE), 2017, : 1425 - 1430
  • [44] Finite-time attitude tracking control for a rigid spacecraft using time-varying terminal sliding mode techniques
    Zhao, Lin
    Jia, Yingmin
    INTERNATIONAL JOURNAL OF CONTROL, 2015, 88 (06) : 1150 - 1162
  • [45] Distributed fixed-time attitude coordinated tracking for multiple rigid spacecraft via a novel integral sliding mode approach
    Sui, Weishun
    Duan, Guangren
    Hou, Mingzhe
    Zhang, Maorui
    JOURNAL OF THE FRANKLIN INSTITUTE-ENGINEERING AND APPLIED MATHEMATICS, 2020, 357 (14): : 9399 - 9422
  • [46] Sliding mode attitude control for flexible spacecraft
    Qi, Wang
    Qin, Wei
    PROCEEDINGS OF THE 2014 INTERNATIONAL CONFERENCE ON MECHATRONICS, CONTROL AND ELECTRONIC ENGINEERING, 2014, 113 : 566 - 570
  • [47] ADAPTIVE SLIDING MODE SPACECRAFT ATTITUDE CONTROL
    Wang, Yizhou
    Chen, Xu
    Tomizuka, Masayoshi
    7TH ANNUAL DYNAMIC SYSTEMS AND CONTROL CONFERENCE, 2014, VOL 2, 2014,
  • [48] ROBUST SLIDING MODE CONTROLLER DESIGN FOR GLOBALLY FAST ATTITUDE TRACKING OF TARGET SPACECRAFT
    Wu, Shunan
    Sun, Zhaowei
    Deng, Hong
    INTERNATIONAL JOURNAL OF INNOVATIVE COMPUTING INFORMATION AND CONTROL, 2011, 7 (5A): : 2087 - 2098
  • [49] Adaptive Nonsingular Terminal Sliding Mode Control for Attitude Tracking of Spacecraft With Actuator Faults
    Jing, Chenghu
    Xu, Hongguang
    Niu, Xinjian
    Song, Xiaoming
    IEEE ACCESS, 2019, 7 : 31485 - 31493
  • [50] Chattering Free Adaptive Sliding Mode Control for Attitude Tracking of Spacecraft with External Disturbance
    Zhang Xuxi
    Liu Xianping
    2014 33RD CHINESE CONTROL CONFERENCE (CCC), 2014, : 2224 - 2228
12345