Robust and optimal attitude control of spacecraft with inertia uncertainties using minimal kinematic parameters

被引：12
|
作者：
Park, Yonmook [1 ]
机构：
[1] FutureRobot Co Ltd, HRI R&D Inst, 1B-905,Uspace 1,660 Daewangpangyo Ro, Songnam 13494, Gyeonggi Do, South Korea
来源：
AEROSPACE SCIENCE AND TECHNOLOGY | 2016年 / 54卷
关键词：
Spacecraft attitude control; Robust control; Optimal control; OPTIMAL STABILIZATION; QUATERNION FEEDBACK; RIGID SPACECRAFT; REGULATOR; SYSTEMS;
D O I：
10.1016/j.ast.2016.04.027
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
In this paper a robust and optimal attitude control design that uses the minimal kinematic parameters and angular velocities feedback is presented for the three-axis attitude stabilization of spacecraft with inertia uncertainties. After proposing a new class of robust attitude control laws for the three-axis attitude stabilization of spacecraft with inertia uncertainties, it is shown that the proposed robust attitude control laws are optimal with respect to performance indices. A numerical example is given to illustrate the theoretical results presented in this paper. (C) 2016 Elsevier Masson SAS. All rights reserved.
引用
收藏
页码：276 / 285
页数：10
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