Fully Actuated Flexible Spacecraft Attitude Control With Input Constraint

被引：0
|
作者：
Wang, Dian [1 ]
Wu, Yun-Hua [1 ]
Yue, Cheng-Fei [2 ,3 ]
Ma, Song-Jing [1 ]
机构：
[1] School of Astronautics, Nanjing University of Aeronautics and Astronautics, Nanjing,211100, China
[2] Institute of Space Science and Applied Technology, Harbin Institute of Technology, Shenzhen,518055, China
[3] National Key Laboratory of Micro-Spacecraft Rapid Design and Intelligent Cluster, Harbin Institute of Technology, Harbin,150001, China
来源：
Zidonghua Xuebao/Acta Automatica Sinica | 2024年 / 50卷 / 11期
关键词：
25;
D O I：
10.16383/j.aas.c230691
中图分类号：
学科分类号：
摘要：
引用
收藏
页码：2177 / 2187
相关论文
共 50 条
  • [31] Robust attitude control of large flexible spacecraft (application of input constrained model predictive control)
    Yamashita, Tetsuo
    Hamada, Yoshiro
    Yamaguchi, Isao
    Nagashio, Tomoyuki
    Kida, Takashi
    Nihon Kikai Gakkai Ronbunshu, C Hen/Transactions of the Japan Society of Mechanical Engineers, Part C, 2013, 79 (802): : 1935 - 1948
  • [32] Recursive dynamic modeling for attitude control of fully flexible spacecraft with central body and appendages
    Wang, Jianyao
    Wang, Hongdong
    ADVANCES IN MECHANICAL ENGINEERING, 2024, 16 (05)
  • [33] Adaptive Attitude Tracking Control of Spacecraft Based on High-Order Fully Actuated System Approach
    Jin, Dongyan
    Hou, Mingyu
    Wang, Tong
    Qiu, Jianbin
    2024 3RD CONFERENCE ON FULLY ACTUATED SYSTEM THEORY AND APPLICATIONS, FASTA 2024, 2024, : 1532 - 1537
  • [34] Autonomous attitude coordinated control for spacecraft formation with input constraint, model uncertainties, and external disturbances
    Song, S. (songshenmin@hit.edu.cn), 1600, Chinese Journal of Aeronautics (27):
  • [35] Autonomous attitude coordinated control for spacecraft formation with input constraint, model uncertainties, and external disturbances
    Zheng Zhong
    Song Shenmin
    CHINESE JOURNAL OF AERONAUTICS, 2014, 27 (03) : 602 - 612
  • [36] Fixed-time Attitude Tracking Control of Rigid Spacecraft With Input Deadzone and Output Constraint
    Zhang, Zhongcai
    Wu, Yuqiang
    2018 37TH CHINESE CONTROL CONFERENCE (CCC), 2018, : 5106 - 5110
  • [37] Quaternion-based Output Feedback Attitude Control for Rigid Spacecraft with Bounded Input Constraint
    Yu Yanbo
    Li Bo
    Hu Qinglei
    2015 34TH CHINESE CONTROL CONFERENCE (CCC), 2015, : 489 - 493
  • [38] Disturbance observer based attitude control for flexible spacecraft with input magnitude and rate constraints
    Liu, Zhijie
    Liu, Jinkun
    Wang, Lijun
    AEROSPACE SCIENCE AND TECHNOLOGY, 2018, 72 : 486 - 492
  • [39] Autonomous attitude coordinated control for spacecraft formation with input constraint,model uncertainties, and external disturbances
    Zheng Zhong
    Song Shenmin
    Chinese Journal of Aeronautics, 2014, (03) : 602 - 612
  • [40] Autonomous attitude coordinated control for spacecraft formation with input constraint,model uncertainties, and external disturbances
    Zheng Zhong
    Song Shenmin
    Chinese Journal of Aeronautics, 2014, 27 (03) : 602 - 612
12345