PASSIVITY-BASED ADAPTIVE ATTITUDE-CONTROL OF A RIGID SPACECRAFT

被引：193
|
作者：
EGELAND, O
GODHAVN, JM
机构：
[1] Norwegian Inst of Technology, Trondheim
来源：
IEEE TRANSACTIONS ON AUTOMATIC CONTROL | 1994年 / 39卷 / 04期
关键词：
D O I：
10.1109/9.286266
中图分类号：
TP [自动化技术、计算机技术];
学科分类号：
0812 ;
摘要：
An adaptive control scheme for the attitude control of a rigid spacecraft is derived using a linear parameterization of the equation of motion. The tracking error is described with the Euler parameter vector. Global convergence of the tracking error to zero is shown using passivity theory. This allows for the use of time-varying positive-definite feedback gain matrices, and the results can easily be extended to other passive parameter update laws.
引用
收藏
页码：842 / 846
页数：5
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