Rotational motion control of a spacecraft

被引：16

作者：

Wisniewski, R ^{[1
]}

Kulczycki, P

机构：

[1] Aalborg Univ, Dept Control Engn, DK-9220 Aalborg, Denmark

[2] Polish Acad Sci, Syst Res Inst, PL-01447 Warsaw, Poland

来源：

IEEE TRANSACTIONS ON AUTOMATIC CONTROL | 2003年 / 48卷 / 04期

关键词：

attitude control; differential geometric methods; nonlinear control; stability theory;

D O I：

10.1109/TAC.2003.809781

中图分类号：

TP [自动化技术、计算机技术];

学科分类号：

0812 ;

摘要：

This note describes a systematic procedure for the control synthesis of a rigid spacecraft using the energy shaping method. The geometric concept of a mechanical system in a coordinate-independent form is used to derive a control algorithm for the Euler-Poincare equations. The main result of this note is a specialization of the method on the unit quaternion group. This note is concluded with the examples of the potential functions and implementation for the three-axis attitude control problem.

引用

页码：643 / 646

页数：4

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