Attitude regulation about a fixed rotation axis

被引：4

作者：

Lawton, J ^{[1
]}

Beard, RW

机构：

[1] Raytheon Syst Inc, Dept Syst Design 2, Tucson, AZ 85734 USA

[2] Brigham Young Univ, Dept Elect & Comp Engn, Provo, UT 84602 USA

来源：

JOURNAL OF GUIDANCE CONTROL AND DYNAMICS | 2003年 / 26卷 / 02期

关键词：

D O I：

10.2514/2.5066

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

The attitude control problem of rotating a rigid body from its current attitude to A desired attitude such that the instantaneous rotation axis is aligned with an externally defined axis of rotation is considered. The key idea is to factor the attitude quaternion into rotations parallel and perpendicular to the desired rotation axis. State feedback and output feedback control strategies are designed to minimize the perpendicular component. Simulation results are provided,to illustrate the salient features of the approach.

引用

页码：253 / 258

页数：6

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