Disturbance-Observer-Based Robust Relative Pose Control for Spacecraft Rendezvous and Proximity Operations Under Input Saturation

被引:76
作者
Sun, Liang [1 ]
Huo, Wei [2 ]
Jiao, Zongxia [2 ]
机构
[1] Univ Sci & Technol Beijing, Sch Automat & Elect Engn, Beijing 100083, Peoples R China
[2] Beihang Univ, Sch Automat Sci & Elect Engn, Sci & Technol Aircraft Control Lab, Beijing 100191, Peoples R China
基金
中国博士后科学基金;
关键词
ATTITUDE TRACKING CONTROL; DYNAMIC SURFACE CONTROL; ACTUATOR SATURATION; NONLINEAR-SYSTEMS; RIGID SPACECRAFT; FEEDBACK-CONTROL; LINEAR-SYSTEMS; POSITION; DESIGN; SYNCHRONIZATION;
D O I
10.1109/TAES.2018.2798239
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
This paper investigates the robust relative pose control for spacecraft rendezvous and proximity operations subject to input saturation, kinematic couplings, parametric uncertainties, and unknown external disturbances. Relative rotational and relative translational nonlinear system models are first derived, and relative attitude and relative position controllers are then proposed, respectively. The kinematic couplings, parametric uncertainties, and unknown external disturbances in dynamical models are treated as compound disturbances, and nonlinear disturbance observers are developed and incorporated into the relative pose control design, which can avoid the assumption on the bounded derivatives of compound disturbances. Meanwhile, input saturation effect of the control torques and forces is compensated by synthesizing the outputs of the auxiliary systems into the controllers. Based on the proposed disturbance observers and auxiliary systems, saturated attitude synchronization and position tracking controllers are developed to reject the unknown compound disturbances and ensure the convergence of the relative pose and velocities. The stability of the closed-loop system is rigorously proved in the Lyapunov framework; relative pose and velocities ultimately converge to the small neighborhoods of the origin in spite of input saturation and model uncertainties. Simulation experiments validate the performance of the proposed robust saturated control strategy.
引用
收藏
页码:1605 / 1617
页数:13
相关论文
共 53 条
[1]  
Bernstein D. S., 2009, MATRIX MATH THEORY F, P110
[2]   Robust adaptive variable structure control of spacecraft under control input saturation [J].
Boskovic, JD ;
Li, SM ;
Mehra, RK .
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2001, 24 (01) :14-22
[3]   Adaptive Fault-Tolerant Spacecraft Attitude Control Design With Transient Response Control [J].
Bustan, Danyal ;
Sani, S. K. Hosseini ;
Pariz, Naser .
IEEE-ASME TRANSACTIONS ON MECHATRONICS, 2014, 19 (04) :1404-1411
[4]   Asymptotic stabilization of linear plants in presence of input and output saturations [J].
Chaoui, FZ ;
Giri, F ;
M'Saad, M .
AUTOMATICA, 2001, 37 (01) :37-42
[5]   Dynamic Surface Control Using Neural Networks for a Class of Uncertain Nonlinear Systems With Input Saturation [J].
Chen, Mou ;
Tao, Gang ;
Jiang, Bin .
IEEE TRANSACTIONS ON NEURAL NETWORKS AND LEARNING SYSTEMS, 2015, 26 (09) :2086-2097
[6]   Disturbance observer based control for nonlinear systems [J].
Chen, WH .
IEEE-ASME TRANSACTIONS ON MECHATRONICS, 2004, 9 (04) :706-710
[7]   Nonlinear disturbance observer-enhanced dynamic inversion control of missiles [J].
Chen, WH .
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2003, 26 (01) :161-166
[8]   TERMINAL GUIDANCE SYSTEM FOR SATELLITE RENDEZVOUS [J].
CLOHESSY, WH ;
WILTSHIRE, RS .
JOURNAL OF THE AEROSPACE SCIENCES, 1960, 27 (09) :653-&
[9]  
Damaren C. J., 2001, P AIAA GUID NAV CONT
[10]   Adaptive Spacecraft Attitude Tracking Control with Actuator Saturation [J].
de Ruiter, Anton. H. J. .
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2010, 33 (05) :1692-1696