Geometric Approach to Spacecraft Attitude Control Using Magnetic and Mechanical Actuation

被引：35

作者：

Forbes, James Richard ^{[1
]}

Damaren, Christopher John ^{[1
]}

机构：

[1] Univ Toronto, Inst Aerosp Studies, Toronto, ON M3H 5T6, Canada

来源：

JOURNAL OF GUIDANCE CONTROL AND DYNAMICS | 2010年 / 33卷 / 02期

关键词：

Attitude control;

D O I：

10.2514/1.46441

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

A geometric approach to spacecraft attitude control using magnetic and mechanical actuation in which the control vector is decomposed into orthogonal and parallel components with respect to the orientation of the instantaneous magnetic field vector is discussed. The attitude of a spacecraft is described by the four parameters.

引用

页码：590 / 595

页数：6

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