A Passive Fault Tolerant Flight Control for Maximum Allowable Vertical Tail Damaged Aircraft-Reference-Cited by-同舟云学术

A Passive Fault Tolerant Flight Control for Maximum Allowable Vertical Tail Damaged Aircraft

Published:2012-03-27 Issue:3 Volume:134 Page:
ISSN:0022-0434
Container-title:Journal of Dynamic Systems, Measurement, and Control
language:en
Short-container-title:

Author:

Li Xiaobo¹²,Liu Hugh H. T.²

Affiliation:

1. Postdoctoal Fellow

2. Flight Systems and Control Group, Institute for Aerospace Studies, University of Toronto, Toronto, ON, M3H 5T6, Canada

Abstract

This paper investigates a passive fault tolerant control to aircraft that suffers from vertical tail damage. A novel notion of damage degree is introduced to parameterize the damaged flight dynamics model. It is applied to seek the maximum allowable damage degree (tolerance capacity) stabilizable by the proposed passive fault tolerant and backup control under a linearized model. The design algorithms are presented and illustrated through numerical simulations on a Boeing-747 100/200 model. Furthermore, the impact of potential control saturation is taken into account in the proposed design and a set of design parameters are tuned such that the maximum allowable damage degree is bounded, represented as the so-called critical damage degree.

Publisher

ASME International

Subject

Computer Science Applications,Mechanical Engineering,Instrumentation,Information Systems,Control and Systems Engineering

Link

http://asmedigitalcollection.asme.org/dynamicsystems/article-pdf/doi/10.1115/1.4005512/5497555/031006_1.pdf

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