Fault diagnosis and fault tolerant control for nonlinear satellite attitude control systems

被引：52

作者：

Gao, Chunyan ^{[1
]}

Duan, Guangren ^{[1
]}

机构：

[1] Harbin Inst Technol, Ctr Control Theory & Guidance Technol, Harbin 150001, Peoples R China

来源：

AEROSPACE SCIENCE AND TECHNOLOGY | 2014年 / 33卷 / 01期

基金：

美国国家科学基金会;

关键词：

Fault diagnosis; Interactive multiple model; Unscented Kalman Filter; Hierarchical structure; Satellite attitude control systems; SENSOR;

D O I：

10.1016/j.ast.2013.12.011

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

In this paper, an integrated fault diagnosis and fault tolerant control scheme is investigated for nonlinear satellite attitude control systems. The fault diagnosis is performed by a novel interactive multiple model approach aiming at reducing the size of the model set. Unknown fault parameters are jointly estimated with system states by state augmentation and a bank of Unscented Kalman Filters. Based on the faulty information obtained from the fault diagnosis system, a proportional-derivative controller is used to recover the faulty system. Simulation results demonstrate the effectiveness of the proposed fault diagnosis and fault tolerant control scheme. (C) 2014 Elsevier Masson SAS. All rights reserved.

引用

页码：9 / 15

页数：7

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