Robust attitude stabilization of spacecraft using minimal kinematic parameters

被引：0

作者：

Park, Y ^{[1
]}

Tahk, MJ ^{[1
]}

机构：

[1] Korea Adv Inst Sci & Technol, Dept Mech Engn, Div Aerosp Engn, Taejon 305701, South Korea

来源：

2001 IEEE INTERNATIONAL CONFERENCE ON ROBOTICS AND AUTOMATION, VOLS I-IV, PROCEEDINGS | 2001年

关键词：

D O I：

暂无

中图分类号：

TP [自动化技术、计算机技术];

学科分类号：

0812 ;

摘要：

In this paper, we consider thc problem of three-axis robust attitude stabilization of a rigid spacecraft using minimal, three-dimensional kinematic parameters. New nonlinear control laws having a class of relaxed feedback gain structures are proposed, and are shown to provide a robustness with respect to inertia uncertainties of a rigid body. A numerical example is given to illustrate the theoretical results.

引用

页码：1621 / 1626

页数：6

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