TIME-VARYING FEEDBACK STABILIZATION OF THE ATTITUDE OF A RIGID SPACECRAFT WITH 2 CONTROLS

被引：97

作者：

MORIN, P ^{[1
]}

SAMSON, C ^{[1
]}

POMET, JB ^{[1
]}

JIANG, ZP ^{[1
]}

机构：

[1] INRIA,F-06902 SOPHIA ANTIPOLIS,FRANCE

来源：

SYSTEMS & CONTROL LETTERS | 1995年 / 25卷 / 05期

关键词：

TIME-VARYING CONTROL; SMOOTH FEEDBACK; ATTITUDE STABILIZATION;

D O I：

10.1016/0167-6911(94)00095-D

中图分类号：

TP [自动化技术、计算机技术];

学科分类号：

0812 ;

摘要：

It is known that rigid body models with two controls cannot be locally asymptotically stabilized by continuous feedbacks which are functions of the state only. This impossibility does no longer hold when the feedback is also a function of time, or when it is discontinuous. A locally stabilizing smooth time-varying feedback is here explicitly derived by using Center Manifold Theory combined with averaging and Lyapunov techniques.

引用

页码：375 / 385

页数：11

共 25 条

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[2]

Brockett R.W, 1983, DIFFERENTIAL GEOMETR

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