Spacecraft Attitude Tracking via Robust Disturbance Observer

被引:0
|
作者
Yan, Ruidong [1 ]
Wu, Zhong [1 ]
机构
[1] Beihang Univ, Sch Instrumentat Sci & Optoelect Engn, Beijing 100191, Peoples R China
基金
中国国家自然科学基金;
关键词
Attitude tracking; Backstepping control; Disturbance observer based control; Robust disturbance observer; RIGID SPACECRAFT; STABILIZATION; SYSTEMS;
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
Previous work has shown that the disturbance observer based control (DOBC) can improve the performance of spacecraft attitude control system for its good disturbance rejection ability. The disturbance rejection ability of DOBC is mainly determined by the disturbance observer. However, the conventional nonlinear disturbance observer for the disturbance with bounded derivative has an estimation error, thus leading to performance degradation. To solve this problem for spacecraft attitude tracking, we propose a composite control scheme. A robust disturbance observer (RDO) is proposed for spacecraft attitude tracking first. RDO not only avoids the re-estimation of spacecraft attitude variables and makes full use of the information of spacecraft dynamics, but also reduces the effects of disturbance model uncertainty on the observer estimation accuracy and achieves finite-time convergence. Second, the composite control scheme is developed by combining RDO with a nonlinear backstepping controller. The disturbance rejection ability of the closed-loop system is improved significantly by compensation of the output of RDO. Finally, numerical simulations are conducted to verify the effectiveness of the proposed method.
引用
收藏
页码:7415 / 7420
页数:6
相关论文
共 50 条
  • [1] Nonlinear disturbance observer-based robust control of attitude tracking of rigid spacecraft
    Lee, Daero
    [J]. NONLINEAR DYNAMICS, 2017, 88 (02) : 1317 - 1328
  • [2] Nonlinear disturbance observer-based robust control of attitude tracking of rigid spacecraft
    Daero Lee
    [J]. Nonlinear Dynamics, 2017, 88 : 1317 - 1328
  • [3] Robust Attitude Tracking Control and Disturbance Rejection for Flexible Spacecraft
    Dong, Hanlin
    Yang, Xuebo
    [J]. PROCEEDINGS OF THE 39TH CHINESE CONTROL CONFERENCE, 2020, : 6947 - 6953
  • [4] Integrated Adaptive Control for Spacecraft Attitude and Orbit Tracking Using Disturbance Observer
    Xia, Kewei
    Eun, Youngho
    Lee, Taeyang
    Park, Sang-Young
    [J]. INTERNATIONAL JOURNAL OF AERONAUTICAL AND SPACE SCIENCES, 2021, 22 (04) : 936 - 947
  • [5] Integrated Adaptive Control for Spacecraft Attitude and Orbit Tracking Using Disturbance Observer
    Kewei Xia
    Youngho Eun
    Taeyang Lee
    Sang-Young Park
    [J]. International Journal of Aeronautical and Space Sciences, 2021, 22 : 936 - 947
  • [6] A fault-tolerant attitude tracking control of spacecraft using an anti-unwinding robust nonlinear disturbance observer
    Amrr, Syed Muhammad
    Nabi, M.
    Tiwari, Pyare Mohan
    [J]. PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2019, 233 (16) : 6005 - 6018
  • [7] Prescribed performance spacecraft attitude tracking with disturbance observer: A performance-adjustable policy
    Niu, Zhaoxiang
    Dai, Ming-Zhe
    Gao, Junyang
    Zhang, Chengxi
    Wu, Jin
    [J]. ADVANCES IN SPACE RESEARCH, 2022, 70 (08) : 2357 - 2368
  • [8] Finite-Time Disturbance Observer Design and Attitude Tracking Control of a Rigid Spacecraft
    Lan, Qixun
    Qian, Chunjiang
    Li, Shihua
    [J]. JOURNAL OF DYNAMIC SYSTEMS MEASUREMENT AND CONTROL-TRANSACTIONS OF THE ASME, 2017, 139 (06):
  • [9] Robust adaptive attitude control of flexible spacecraft using a sliding mode disturbance observer
    Javaid, Umair
    Zhen, Ziyang
    Xue, Yixuan
    Ijaz, Salman
    [J]. PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2022, 236 (11) : 2235 - 2253
  • [10] Robust approach for attitude tracking and nonlinear disturbance rejection of rigid body spacecraft
    Ping, Zhaowu
    Dong, Yi
    Tang, Hao
    Lu, Jun-Guo
    [J]. IET CONTROL THEORY AND APPLICATIONS, 2016, 10 (17): : 2325 - 2330