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
  • [1] Fuzzy sliding mode controller design for satellite attitude tracking
    Lu, Jian-Ting
    Ma, Guang-Fu
    Li, Chuan-Jiang
    Jilin Daxue Xuebao (Gongxueban)/Journal of Jilin University (Engineering and Technology Edition), 2007, 37 (04): : 955 - 958
  • [2] PD Integrated Sliding Mode Controller design for Attitude Tracking Control of Rigid Body Spacecraft
    Javaid, Umair
    Razzaq, Muhammad Junaid
    Rafique, Syed Furquan
    PROCEEDINGS OF 2019 16TH INTERNATIONAL BHURBAN CONFERENCE ON APPLIED SCIENCES AND TECHNOLOGY (IBCAST), 2019, : 537 - 542
  • [3] Sliding Mode Controller for Satellite Attitude Stabilization Maneuver
    Feng, Licheng
    Chen, Xiaoqian
    Sheng, Tao
    PROCEEDINGS OF THE 3RD INTERNATIONAL CONFERENCE ON MECHANICAL ENGINEERING AND INTELLIGENT SYSTEMS (ICMEIS 2015), 2015, 26 : 854 - 858
  • [4] Sliding mode attitude tracking of rigid spacecraft with disturbances
    Lu, Kunfeng
    Xia, Yuanqing
    Zhu, Zheng
    Basin, Michael V.
    JOURNAL OF THE FRANKLIN INSTITUTE-ENGINEERING AND APPLIED MATHEMATICS, 2012, 349 (02): : 413 - 440
  • [5] SLIDING-MODE CONTROLLER-DESIGN FOR SPACECRAFT ATTITUDE TRACKING MANEUVERS
    CHEN, YP
    LO, SC
    IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, 1993, 29 (04) : 1328 - 1333
  • [6] Fuzzy Sliding Mode Controller Design for Spacecraft Attitude Tracking in Terms of Quaternion
    Mohammad, Ataei
    Ehsan, Shafiei S.
    PROCEEDINGS OF THE 27TH CHINESE CONTROL CONFERENCE, VOL 3, 2008, : 753 - +
  • [7] Sliding Mode Control for a Satellite Attitude Tracking System
    Gao, Dai
    Lv, Jianting
    2008 2ND INTERNATIONAL SYMPOSIUM ON SYSTEMS AND CONTROL IN AEROSPACE AND ASTRONAUTICS, VOLS 1 AND 2, 2008, : 865 - 868
  • [8] Attitude Control of a Rigid Satellite with Event -triggered Sliding Mode
    Das, Gargi
    Patra, Nilanjan
    Mishra, Rajiv Kumar
    IFAC PAPERSONLINE, 2022, 55 (22): : 346 - 351
  • [9] Sliding mode attitude controller design for nonlinear flexible geosynchronous satellite with thrust jets
    Abdulhamitbilal, Erkan
    Jafarov, Elbrous M.
    2008 INTERNATIONAL WORKSHOP ON VARIABLE STRUCTURE SYSTEMS, 2008, : 221 - 226
  • [10] 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
12345