Model Predictive Sliding Control for Finite-Time Three-Axis Spacecraft Attitude Tracking

被引:79
作者
Bayat, Farhad [1 ]
机构
[1] Univ Zanjan, Dept Engn, Zanjan 4537138791, Iran
关键词
Model predictive control; nonsingular sliding mode control; spacecraft attitude control; RIGID SPACECRAFT; DESIGN; STABILIZATION; ROBUST;
D O I
10.1109/TIE.2018.2881936
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
This paper deals with the robust optimal three-axis attitude tracking problem of spacecrafts. To this aim, the exceptional features of two advanced control approaches, i.e., nonlinear terminal sliding mode control (TSMC) and linear model predictive control (MPC), are combined in a compound double layer structure. The proposed approach addresses the global stability and robust attitude tracking of near-polar orbit spacecrafts actuated by a set of reaction wheels and subject to unknown disturbances, uncertainties, and actuators' saturation. The TSMC controller is designed to guarantee the robust three-axis attitude tracking goal in the presence of disturbances and uncertainties provided that proper target points are available. The next part of the compound controller takes the advantages of the MPC technique (i.e., preknown attitude maneuvers and constraints) into account to provide the required optimal target points for the lower level TSMC controller. Despite the fact that the spacecraft has nonlinear nature, we have analytically derived conditions under which the actuators' constraints satisfaction is guaranteed a priori. Finally, a set of simulation results are provided to illustrate the effectiveness and performance of the proposed method.
引用
收藏
页码:7986 / 7996
页数:11
相关论文
共 50 条
[21]   Finite-time attitude tracking control for a rigid spacecraft using time-varying terminal sliding mode techniques [J].
Zhao, Lin ;
Jia, Yingmin .
INTERNATIONAL JOURNAL OF CONTROL, 2015, 88 (06) :1150-1162
[22]   Robust Adaptive Finite-Time Prescribed Performance Attitude Tracking Control of Spacecraft [J].
Yao, Qijia .
INTERNATIONAL JOURNAL OF AERONAUTICAL AND SPACE SCIENCES, 2021, 22 (05) :1183-1193
[23]   adaptive backstepping finite-time attitude tracking control of spacecraft without unwinding [J].
Huang, Bing ;
Li, Aijun ;
Guo, Yong ;
Wang, Changqing ;
YuanZhang .
PROCEEDINGS OF THE 36TH CHINESE CONTROL CONFERENCE (CCC 2017), 2017, :1180-1185
[24]   A novel finite-time prescribed performance control scheme for spacecraft attitude tracking [J].
Gao, Shihong ;
Liu, Xiaoping ;
Jing, Yuanwei ;
Dimirovski, Georgi M. .
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 118
[25]   Finite-time distributed cooperative attitude tracking control for multiple rigid spacecraft [J].
He, Xiaoyan ;
Wang, Qingyun ;
Yu, Wenwu .
APPLIED MATHEMATICS AND COMPUTATION, 2015, 256 :724-734
[26]   Finite-time attitude tracking control for spacecraft without angular velocity measurements [J].
Yuan, Li ;
Ma, Guangfu ;
Li, Chuanjiang ;
Jiang, Boyan .
JOURNAL OF SYSTEMS ENGINEERING AND ELECTRONICS, 2017, 28 (06) :1174-1185
[27]   FINITE-TIME ATTITUDE TRACKING CONTROL FOR SPACECRAFT WITHOUT ANGULAR VELOCITY MEASUREMENT [J].
Jiang, Boyan ;
Li, Chuanjiang ;
Guo, Yanning ;
Dong, Hongyang .
SPACEFLIGHT MECHANICS 2017, PTS I - IV, 2017, 160 :2591-2602
[28]   Finite-time attitude-tracking control for rigid spacecraft with actuator failures and saturation constraints [J].
Gao, Shihong ;
Jing, Yuanwei ;
Liu, Xiaoping ;
Zhang, Siying .
INTERNATIONAL JOURNAL OF ROBUST AND NONLINEAR CONTROL, 2020, 30 (05) :1903-1937
[29]   Finite-Time Anti-Disturbance Inverse Optimal Attitude Tracking Control of Flexible Spacecraft [J].
Pukdeboon, Chutiphon ;
Jitpattanakul, Anuchit .
MATHEMATICAL PROBLEMS IN ENGINEERING, 2013, 2013
[30]   Robust non-aggressive three-axis attitude control of spacecraft: dynamic sliding mode approach [J].
Nikyar, Javad ;
Bayat, Farhad ;
Mohammadkhani, Mohammadali .
CONTROL THEORY AND TECHNOLOGY, 2023, 21 (04) :505-514