Finite-time attitude tracking control for spacecraft without angular velocity measurements

被引：4
|
作者：
Yuan, Li [1 ]
Ma, Guangfu [1 ]
Li, Chuanjiang [1 ]
Jiang, Boyan [1 ]
机构：
[1] Harbin Inst Technol, Dept Control Sci & Engn, Harbin 150001, Heilongjiang, Peoples R China
来源：
JOURNAL OF SYSTEMS ENGINEERING AND ELECTRONICS | 2017年 / 28卷 / 06期
基金：
中国国家自然科学基金;
关键词：
output feedback; spacecraft attitude stabilization; finite-time control; TERMINAL SLIDING MODE; RIGID SPACECRAFT; OUTPUT-FEEDBACK; NONLINEAR-SYSTEMS; STABILIZATION; DISTURBANCES;
D O I：
10.21629/JSEE.2017.06.15
中图分类号：
TP [自动化技术、计算机技术];
学科分类号：
0812 ;
摘要：
The output feedback control for spacecraft attitude tracking system is investigated in this study. It is assumed that angular velocity measurements are not available for feedback control. A technique named adding power integrator (API) is adopted to estimate the pseudo-angular-velocity. Then we design a finite-time attitude control law, which only utilizes the relative attitude information. The stability analyses of the feedback system are proved as well, which shows the attitude tracking errors will converge into a region of zero even the external disturbances exist. The simulation results illustrate the high precision and robust attitude control performance of the proposed control strategy.
引用
收藏
页码：1174 / 1185
页数：12
相关论文
共 50 条
  • [1] Finite-time attitude tracking control for spacecraft without angular velocity measurements
    Li Yuan
    Guangfu Ma
    Chuanjiang Li
    Boyan Jiang
    [J]. Journal of Systems Engineering and Electronics, 2017, 28 (06) : 1174 - 1185
  • [2] FINITE-TIME ATTITUDE TRACKING CONTROL FOR SPACECRAFT WITHOUT ANGULAR VELOCITY MEASUREMENT
    Jiang, Boyan
    Li, Chuanjiang
    Guo, Yanning
    Dong, Hongyang
    [J]. SPACEFLIGHT MECHANICS 2017, PTS I - IV, 2017, 160 : 2591 - 2602
  • [3] Finite-time Attitude Tracking for Fully-actuated Flexible Spacecraft without Angular Velocity Measurements
    Huang, Qin
    Zhang, Ying
    [J]. 2023 2ND CONFERENCE ON FULLY ACTUATED SYSTEM THEORY AND APPLICATIONS, CFASTA, 2023, : 1061 - 1066
  • [4] Finite-time Attitude Tracking for Spacecraft With Unknown Boundary Disturbance and Angular Velocity
    Qin, Huang
    Ying, Zhang
    Rui, Zhang
    [J]. PROCEEDINGS OF THE 39TH CHINESE CONTROL CONFERENCE, 2020, : 6990 - 6995
  • [5] Finite-time sliding mode attitude control for rigid spacecraft without angular velocity measurement
    Shao, Shikai
    Zong, Qun
    Tian, Bailing
    Wang, Fang
    [J]. JOURNAL OF THE FRANKLIN INSTITUTE-ENGINEERING AND APPLIED MATHEMATICS, 2017, 354 (12): : 4656 - 4674
  • [6] Fixed-Time Attitude Tracking Control for Rigid Spacecraft Without Angular Velocity Measurements
    Zou, An-Min
    Fan, Zhun
    [J]. IEEE TRANSACTIONS ON INDUSTRIAL ELECTRONICS, 2020, 67 (08) : 6795 - 6805
  • [7] Relative position finite-time coordinated tracking control of spacecraft formation without velocity measurements
    Hu, Qinglei
    Zhang, Jian
    [J]. ISA TRANSACTIONS, 2015, 54 : 60 - 74
  • [8] adaptive backstepping finite-time attitude tracking control of spacecraft without unwinding
    Huang, Bing
    Li, Aijun
    Guo, Yong
    Wang, Changqing
    YuanZhang
    [J]. PROCEEDINGS OF THE 36TH CHINESE CONTROL CONFERENCE (CCC 2017), 2017, : 1180 - 1185
  • [9] Continuous Finite-Time Attitude Control for Rigid Spacecraft Based on Angular Velocity Observer
    Hu, Qinglei
    Jiang, Boyan
    [J]. IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, 2018, 54 (03) : 1082 - 1092
  • [10] Global saturated velocity-free finite-time control for attitude tracking of spacecraft
    Xia, Yuquan
    Su, Yuxin
    [J]. IET CONTROL THEORY AND APPLICATIONS, 2019, 13 (11): : 1591 - 1602
12345