Adaptive Fault-Tolerant Control for HSV With Unknown Control Direction

被引：36

作者：

Xu, Binyan ^{[1
]}

Qi, Ruiyun ^{[1
]}

Jiang, Bin ^{[1
]}

机构：

[1] Nanjing Univ Aeronaut & Astronaut, Coll Automat Engn, Nanjing 210016, Peoples R China

来源：

IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS | 2019年 / 55卷 / 06期

基金：

中国国家自然科学基金;

关键词：

Vehicle dynamics; Fault tolerance; Fault tolerant systems; Elevators; Control systems; Aerodynamics; Adaptation models; Adaptive control; antiwindup control; fault-tolerant control; hypersonic vehicle; Nussbaum gain function; OUTPUT-FEEDBACK CONTROL; NONLINEAR-SYSTEMS; TRACKING CONTROL; HYPERSONIC VEHICLES; DESIGN;

D O I：

10.1109/TAES.2019.2894918

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

This paper proposes an adaptive antiwindup fault-tolerant control system for a hypersonic vehicle with parametric uncertainties. Not only the loss-of-effectiveness and stuck-type elevator fault, but also the reverse-type fault causing the uncertainty of control direction is considered. The fault-tolerant controller designed through feedback linearization is combined with an online parameter estimator and a Nussbaum gain function, so that the uncertainties can be estimated adaptively. An antiwindup compensator is introduced to the control system to handle the input constraints.

引用

页码：2743 / 2758

页数：16

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