Youla Parameterization Fault-Tolerant Controller Design for Aircraft

被引：5

作者：

Cui, Lei ^{[1
]}

Liu, Hongyuan ^{[1
]}

Yang, Ying ^{[1
]}

机构：

[1] Peking Univ, State Key Lab Turbulence & Complex Syst, Dept Mech & Aerosp Engn, Coll Engn, Beijing 100871, Peoples R China

来源：

JOURNAL OF GUIDANCE CONTROL AND DYNAMICS | 2013年 / 36卷 / 05期

基金：

中国国家自然科学基金;

关键词：

Aircraft landing - VTOL/STOL aircraft - Fault tolerance - Controllers - Parameterization - Aircraft detection;

D O I：

10.2514/1.57991

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

A study was conducted to show the capability and viability of the proposed Youla parameterization fault-tolerant controller on a realistic vertical takeoff and landing aircraft model and to enhance critical flight safety issues. The simulation results demonstrate the tracking performance is guaranteed in a faulty situation, the stability of faulty vertical takeoff and landing aircraft is ensured, and the actuator fault can be well reconstructed. Therefore, the proposed Youla parameterization fault-tolerant controller is effective for aircraft control. The simulation result has successfully demonstrated the effectiveness of the reconfigurable fault-parameterized matrix.

引用

页码：1533 / 1538

页数：6

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