Controllability of Spacecraft Using Only Magnetic Torques

被引：29
|
作者：
Yang, Yaguang [1 ]
机构：
[1] US Nucl Regulatory Commiss, Rockville, MD USA
来源：
IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS | 2016年 / 52卷 / 02期
关键词：
ATTITUDE-CONTROL;
D O I：
10.1109/TAES.2015.150520
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
Spacecraft attitude control using only magnetic torques is a time-varying system. Many designs have been proposed using linear quadratic regulator (LQR) and H-infinity formulations. The existence of the solutions depends on the controllability of the linear time-varying systems, which has not been established. In this paper, the conditions of controllability for this linear time-varying system is derived.
引用
收藏
页码：954 / U44
页数：8
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