A simple velocity-free controller for attitude regulation of a spacecraft with delayed feedback

被引：45

作者：

Ailon, A

Segev, R

Arogeti, S

机构：

[1] Ben Gurion Univ Negev, Dept Elect & Comp Engn, IL-84105 Beer Sheva, Israel

[2] Ben Gurion Univ Negev, Dept Mech Engn, IL-84105 Beer Sheva, Israel

来源：

IEEE TRANSACTIONS ON AUTOMATIC CONTROL | 2004年 / 49卷 / 01期

关键词：

attitude regulation; exponential stability; region of attraction; spacecraft; time-delay; velocity-free controller;

D O I：

10.1109/TAC.2003.821406

中图分类号：

TP [自动化技术、计算机技术];

学科分类号：

0812 ;

摘要：

In this note, we consider the application of a velocity-free controller for attitude regulation of a rigid spacecraft with gas jet actuators when the effects of time-delays in the feedback loop are taken into consideration. Simple sufficient conditions for exponential stability are presented. Some structural properties of the resulting closed-loop system are studied, and relevant design tools are demonstrated.

引用

页码：125 / 130

页数：6

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