Anti-Unwinding Sliding Mode Control for Rigid Spacecraft Based on Modified Rodrigues Parameters

Dong，Rui Qi1; Wu，Ai Guo1; Zhang，Ying1; Duan，Guang Ren2; Huang，Jing3

2022

10.1109/TAES.2022.3218277

IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS   Impact Factor & Quartile

0018-9251

1557-9603

In this paper, attitude maneuver control without unwinding phenomenon is investigated for rigid spacecraft via modified Rodrigues parameters. A novel switching function is constructed by a hyperbolic sine function to guarantee that the sliding surface contains two stable equilibria. A sliding mode controller is developed to ensure that the sliding surface is reachable. Moreover, a dynamic parameter is designed to guarantee unwinding-free performance of the closed-loop system when the system states outside the sliding surface. In addition, a boundary layer is introduced to deal with the chattering problem. Further, the unwinding-free performance within the boundary layer is guaranteed by imposing some conditions on the parameters of the switching function. Finally, comparison simulations are performed to verify the effectiveness and superiority of the presented control law.

Aerodynamics Angular velocity Anti-unwinding Attitude control Materials requirements planning Modified Rodrigues parameters Rigid spacecraft Sliding mode control Sliding mode control Space vehicles Switches

EI

English

Others

20224613110237

Backstepping ; Boolean functions ; Boundary layers ; Closed loop systems ; Hyperbolic functions ; Rotation ; Sliding mode control ; Switching functions

Computer Theory, Includes Formal Logic, Automata Theory, Switching Theory, Programming Theory:721.1 ; Control Systems:731.1 ; Specific Variables Control:731.3 ; Mathematics:921 ; Algebra:921.1 ; Mechanics:931.1 ; Systems Science:961

ENGINEERING

2-s2.0-85141625238

Scopus

1.School of Mechanical Engineering and Automation, Harbin Institute of Technology (Shenzhen), Shenzhen, P. R. China
2.Center for Control Science and Technology, Southern University of Science and Technology, Shenzhen, P. R. China
3.Shanghai Aerospace Control Technology Institute, Shanghai, China

Dong，Rui Qi,Wu，Ai Guo,Zhang，Ying,et al. Anti-Unwinding Sliding Mode Control for Rigid Spacecraft Based on Modified Rodrigues Parameters[J]. IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS,2022,PP(99):1-13.

Dong，Rui Qi,Wu，Ai Guo,Zhang，Ying,Duan，Guang Ren,&Huang，Jing.(2022).Anti-Unwinding Sliding Mode Control for Rigid Spacecraft Based on Modified Rodrigues Parameters.IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS,PP(99),1-13.

Dong，Rui Qi,et al."Anti-Unwinding Sliding Mode Control for Rigid Spacecraft Based on Modified Rodrigues Parameters".IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS PP.99(2022):1-13.