QUATERNION-BASED RATE ATTITUDE TRACKING SYSTEM WITH APPLICATION TO GIMBAL ATTITUDE-CONTROL

被引：30
作者：
WEISS, H
机构：
[1] Rafael, Haifa
来源：
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS | 1993年 / 16卷 / 04期
关键词：
D O I：
10.2514/3.21057
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
The paper deals with rate and attitude control of a rigid body. The discussed control system contains an inner velocity loop that tracks the desired rate command and an outer attitude loop that tracks the desired attitude command. The control algorithm uses quaternions as a measure of attitude errors to achieve tracking via instantaneous eigenaxis rotation. The paper discusses the stability of the new algorithm and presents its application to multiaxis gimbal attitude control.
引用
收藏
页码：609 / 616
页数：8
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