Nonlinear attitude tracking control for spacecraft formation with multiple delays

被引：27
|
作者：
Yang, Hongjiu [1 ]
You, Xiu [1 ]
Xia, Yuanqing [2 ]
Liu, Zhixin [1 ]
机构：
[1] Yanshan Univ, Coll Elect Engn, Qinhuangdao 066004, Peoples R China
[2] Beijing Inst Technol, Sch Automat, Beijing 100081, Peoples R China
来源：
ADVANCES IN SPACE RESEARCH | 2014年 / 54卷 / 04期
基金：
中国国家自然科学基金;
关键词：
Spacecraft formulation; Attitude tracking; Nonlinear control; Adaptive control; Multiple delays; DISTURBANCE REJECTION CONTROL; SLIDING MODE CONTROL; FLEXIBLE SPACECRAFT; SYNCHRONIZATION; SYSTEMS; COORDINATION; CONSENSUS;
D O I：
10.1016/j.asr.2014.04.026
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
This paper addresses the attitude tracking control for spacecraft formation with delay free and communication delays. With help of the idea of sliding control, an adaptive attitude synchronization control architecture is established. Furthermore, by introducing a nonsmooth feedback function, a new class of nonlinear controllers for the attitude tracking of spacecraft is developed. Both parameter uncertainties and unknown external disturbances are dealt with via the kind of controllers. Finally, some simulation results are given to demonstrate the effectiveness and advantages of the proposed results. (C) 2014 COSPAR. Published by Elsevier Ltd. All rights reserved.
引用
收藏
页码：759 / 769
页数：11
相关论文
共 50 条
  • [21] Coordinated Multiple Spacecraft Attitude Control with Communication Time Delays and Uncertainties
    Li Guiming
    Liu Liangdong
    CHINESE JOURNAL OF AERONAUTICS, 2012, 25 (05) : 698 - 708
  • [22] Coordinated Multiple Spacecraft Attitude Control with Communication Time Delays and Uncertainties
    LI Guiminga
    Chinese Journal of Aeronautics , 2012, (05) : 698 - 708
  • [23] Robust Nonlinear Attitude Tracking for Rigid Spacecraft with Constrained Control Inputs
    Sun, Liang
    Zhu, Bing
    2018 3RD IEEE INTERNATIONAL CONFERENCE ON ADVANCED ROBOTICS AND MECHATRONICS (IEEE ICARM), 2018, : 225 - 229
  • [24] NONLINEAR DISTURBANCE REJECTION OF NANO-SPACECRAFT ATTITUDE TRACKING CONTROL
    Qin, Changmao
    Qiu, Qunhai
    Wen, Jianhua
    FOURTH IAA CONFERENCE ON DYNAMICS AND CONTROL OF SPACE SYSTEMS 2018, PTS I-III, 2018, 165 : 1007 - 1017
  • [25] Nonlinear attitude tracking control of a spacecraft with thrusters based on error quaternions
    Jing, Wu-Xing
    Xu, Shi-Jie
    Jing, W.-X. (wuxingjing@hotmail.com), 1600, Chinese Journal of Aeronautics (15): : 129 - 138
  • [26] Nonlinear Model Predictive Control for Spacecraft Attitude Tracking with Kalman Filter
    Li, Dong-Ting
    Wu, Ai-Guo
    Li, Peng
    2020 CHINESE AUTOMATION CONGRESS (CAC 2020), 2020, : 3389 - 3394
  • [27] Synchronized Fault-tolerant Attitude Control for Spacecraft Formation with Communication Delays
    Zhang, Jian
    Wu, Wenjie
    Liu, Long
    Xie, Wenbo
    2020 CHINESE AUTOMATION CONGRESS (CAC 2020), 2020, : 597 - 602
  • [28] Robust attitude tracking control for a rigid spacecraft under input delays and actuator errors
    Safa, Alireza
    Baradarannia, Mehdi
    Kharrati, Flamed
    Khanmohammadi, Sohrab
    INTERNATIONAL JOURNAL OF CONTROL, 2019, 92 (05) : 1183 - 1195
  • [29] Distributed Adaptive Sliding Mode Control for Attitude Tracking of Multiple Spacecraft
    Yang Dapeng
    Liu Xiangdong
    Li Zhongkui
    Guo Yaohua
    2013 32ND CHINESE CONTROL CONFERENCE (CCC), 2013, : 6917 - 6922
  • [30] Distributed attitude coordinated tracking control for spacecraft formation with state constraints
    Wang W.-J.
    Li C.-J.
    Sun Y.-C.
    Ma G.-F.
    Kongzhi yu Juece/Control and Decision, 2018, 33 (09): : 1584 - 1590
12345