Robust control of the missile attitude based on quaternion feedback

被引：44

作者：

Song, Chanho ^{[1
]}

Kim, Sang-Jae ^{[1
]}

Kim, Seung-Hwan ^{[1
]}

Nam, H. S. ^{[1
]}

机构：

[1] Agcy Def Dev, Taejon 305600, South Korea

来源：

CONTROL ENGINEERING PRACTICE | 2006年 / 14卷 / 07期

关键词：

quaternion feedback; attitude control; uncertainty; stability analysis;

D O I：

10.1016/j.conengprac.2005.04.003

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 paper, a robust control scheme based on the quaternion feedback for attitude control of missiles employing thrust vector control is proposed. The control law consists of two parts: the nominal feedback part and an additional term for ensuring robustness to the plant uncertainties. For the proposed control scheme, a stability analysis is given and the performance is shown via computer simulation. (c) 2005 Elsevier Ltd. All rights reserved.

引用

页码：811 / 818

页数：8

共 9 条

[1] A NEW CLASS OF STABILIZING CONTROLLERS FOR UNCERTAIN DYNAMICAL-SYSTEMS [J].