Nonlinear robust adaptive trajectory tracking control for spacecraft proximity operations

被引:6
|
作者
Sun, Liang [1 ]
Huo, Wei [1 ]
机构
[1] Beihang Univ, Sci & Technol Aircraft Control Lab, Div Res 7, Beijing 100191, Peoples R China
关键词
Spacecraft control; proximity operations; trajectory tracking; nonlinear control; adaptive control; modeling uncertainties; RIGID SPACECRAFT; ATTITUDE-CONTROL; POSITION; DOCKING;
D O I
10.1177/0954410015577996
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Six degrees of freedom (6DOF) relative motion trajectory tracking control is studied for a chaser spacecraft with parametric uncertainties and external disturbances to approach a tumbling target in deep space. After modeling the nonlinear and coupled relative motion dynamics in the chaser body-fixed frame, reference trajectories of the relative attitude and relative position are designed, then a 6DOF integrated trajectory tracking controller is developed based on a robust adaptive method. Asymptotic stability of the 6DOF closed-loop system is derived within the Lyapunov framework. The performance of proposed controller is demonstrated through a numerical simulation example.
引用
收藏
页码:2429 / 2440
页数:12
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