Finite-time output feedback attitude control of spacecraft

被引：0
|
作者：
Gao, Dai [1 ]
Lu, Jianting [2 ]
Wang, Benli [1 ]
机构：
[1] Research Center of Satellite Technology, Harbin Institute of Technology, Harbin 150080, China
[2] School of Mathematical Sciences, Heilongjiang University, Harbin 150080, China
来源：
Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica | 2012年 / 33卷 / 11期
关键词：
D O I：
暂无
中图分类号：
学科分类号：
摘要：
引用
收藏
页码：2074 / 2081
相关论文
共 50 条
  • [1] Attitude output feedback control for rigid spacecraft with finite-time convergence
    Hu, Qinglei
    Niu, Guanglin
    ISA TRANSACTIONS, 2017, 70 : 173 - 186
  • [2] Saturated output feedback control for finite-time attitude stabilization of spacecraft
    Xia, Yuquan
    Su, Yuxin
    PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART C-JOURNAL OF MECHANICAL ENGINEERING SCIENCE, 2020, 234 (23) : 4557 - 4571
  • [3] Finite-time output feedback control for the attitude of the spacecraft without unwinding
    Guo, Yong
    Song, Shen-Min
    Li, Xue-Hui
    Zhu, Zhibin
    PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2018, 232 (08) : 1421 - 1433
  • [4] Finite-Time Output Feedback Attitude Tracking Control for Rigid Spacecraft
    Zou, An-Min
    IEEE TRANSACTIONS ON CONTROL SYSTEMS TECHNOLOGY, 2014, 22 (01) : 338 - 345
  • [5] Finite-time output feedback attitude synchronization for multiple spacecraft
    Zong, Qun
    Shao, Shikai
    Tian, Bailing
    Zhang, Xiuyun
    Liu, Wenjing
    TRANSACTIONS OF THE INSTITUTE OF MEASUREMENT AND CONTROL, 2018, 40 (10) : 3023 - 3039
  • [6] Bounded finite-time attitude tracking control for rigid spacecraft via output feedback
    Zhang, Jian
    Hu, Qinglei
    Wang, Danwei
    AEROSPACE SCIENCE AND TECHNOLOGY, 2017, 64 : 75 - 84
  • [7] Bounded Finite-Time Coordinated Attitude Control via Output Feedback for Spacecraft Formation
    Hu, Qinglei
    Zhang, Jian
    JOURNAL OF AEROSPACE ENGINEERING, 2015, 28 (05)
  • [8] Finite-time output feedback attitude control for rigid spacecraft under control input saturation
    Zou, An-Mm
    de Ruiter, Anton H. J.
    Kumar, Krishna Dev
    JOURNAL OF THE FRANKLIN INSTITUTE-ENGINEERING AND APPLIED MATHEMATICS, 2016, 353 (17): : 4442 - 4470
  • [9] Finite-time output feedback attitude control for spacecraft using "Adding a power integrator" technique
    Jiang, Boyan
    Li, Chuanjiang
    Ma, Guangfu
    AEROSPACE SCIENCE AND TECHNOLOGY, 2017, 66 : 342 - 354
  • [10] Finite-time Output Feedback Control of Spacecraft Attitude Based on "Adding a Power Integrator" Method
    Jiang, Boyan
    Li, Chuanjiang
    Yuan, Li
    Guangfu
    2017 29TH CHINESE CONTROL AND DECISION CONFERENCE (CCDC), 2017, : 6337 - 6342
12345