Sliding Mode Controller Design for Rigid Satellite Attitude Tracking

被引：3
|
作者：
Wu, Shunan [1 ]
Sun, Zhaowei [2 ]
Li, Hui [2 ]
机构：
[1] Harbin Inst Technol, Res Ctr Satellite Technol, Harbin 150001, Peoples R China
[2] Harbin Inst Technol, Harbin 150001, Peoples R China
来源：
2009 IEEE INTERNATIONAL CONFERENCE ON ROBOTICS AND BIOMIMETICS (ROBIO 2009), VOLS 1-4 | 2009年
关键词：
SPACECRAFT; ROBUST;
D O I：
10.1109/ROBIO.2009.5420472
中图分类号：
TP18 [人工智能理论];
学科分类号：
081104 ; 0812 ; 0835 ; 1405 ;
摘要：
The problem of attitude tracking control for rigid satellite is studied in this paper. Based on the dynamic equation and kinematics equation using error quaternion and error angular velocity, a sliding mode controller is initially designed to solve this problem. In order to avoid inherent chattering of sliding mode control and then improve control effect, a disturbance observer is introduced and included in the modified controller. The convergence of both controllers are respectively proved theoretically. Simulations are finally performed and the results demonstrate the performance of proposed controllers.
引用
收藏
页码：2238 / +
页数：2
相关论文
共 50 条
  • [21] Attitude tracking control model design for rigid spacecrafts based on discrete-time sliding mode
    Wen, Weibin
    Fu, Qiang
    Wang, Fang
    Xiao, Yuan
    Wang, Tao
    Harbin Gongye Daxue Xuebao/Journal of Harbin Institute of Technology, 2015, 47 (03): : 8 - 14
  • [22] Adaptive Attitude Controller Design for a Rigid Satellite with Feedback Linearization Approach
    Akram Adnane
    Abdellatif Bellar
    Mohammed Arezki Si Mohammed
    Jiang Hong
    Zoubir Ahmed Foitih
    The Journal of the Astronautical Sciences, 2020, 67 : 1445 - 1469
  • [23] Adaptive Attitude Controller Design for a Rigid Satellite with Feedback Linearization Approach
    Adnane, Akram
    Bellar, Abdellatif
    Mohammed, Mohammed Arezki Si
    Hong, Jiang
    Foitih, Zoubir Ahmed
    JOURNAL OF THE ASTRONAUTICAL SCIENCES, 2020, 67 (04): : 1445 - 1469
  • [24] A Micro-satellite Attitude System Using Sliding Mode Observer and Sliding Mode Controller with Perturbation Estimation
    Cheng, Yuehua
    Jiang, Bin
    Zhang, Xian
    2008 2ND INTERNATIONAL SYMPOSIUM ON SYSTEMS AND CONTROL IN AEROSPACE AND ASTRONAUTICS, VOLS 1 AND 2, 2008, : 884 - +
  • [25] Finite Time Sliding Mode Controller for a Rigid Satellite in Presence of Actuator Failure
    Yadegari, Hamed
    Chao, Han
    Zhu Yukai
    2016 3RD INTERNATIONAL CONFERENCE ON INFORMATION SCIENCE AND CONTROL ENGINEERING (ICISCE), 2016, : 1327 - 1331
  • [26] A de-coupled sliding mode controller and observer for satellite attitude control
    McDuffie, JH
    Shtessel, YB
    PROCEEDINGS OF THE TWENTY-NINTH SOUTHEASTERN SYMPOSIUM ON SYSTEM THEORY, 1997, : 92 - 97
  • [27] Dynamic Sliding Mode Controller with Variable Structure for Fast Satellite Attitude Maneuver
    Gao Shan
    Li You
    Xue Huifeng
    Yao ShuYue
    MATHEMATICAL PROBLEMS IN ENGINEERING, 2021, 2021
  • [28] A de-coupled sliding mode controller and observer for satellite attitude control
    McDuffie, JH
    Shtessel, YB
    PROCEEDINGS OF THE 1997 AMERICAN CONTROL CONFERENCE, VOLS 1-6, 1997, : 564 - 565
  • [29] A New Nonsingular Terminal Sliding Mode Control for Rigid Spacecraft Attitude Tracking
    Wang, Zeng
    Su, Yuxin
    Zhang, Liyin
    JOURNAL OF DYNAMIC SYSTEMS MEASUREMENT AND CONTROL-TRANSACTIONS OF THE ASME, 2018, 140 (05):
  • [30] Time-varying sliding mode controls in rigid spacecraft attitude tracking
    Jin Yongqiang
    Liu Xiangdong
    Qiu Wei
    Hou Chaozhen
    CHINESE JOURNAL OF AERONAUTICS, 2008, 21 (04) : 352 - 360
12345