AIRCRAFT CONTROL LAW RECONFIGURATION-Reference-Cited by-同舟云学术

AIRCRAFT CONTROL LAW RECONFIGURATION

Published:2015-03-30 Issue:1 Volume:19 Page:14-18
ISSN:1648-7788
Container-title:Aviation
language:
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Author:

Kosyanchuk Vladislav¹,Selvesyuk Nikolay¹,Kulchak Alexey¹

Affiliation:

1. State Research Institute of Aviation Systems

Abstract

The synthesis of MIMO fault-tolerant control systems under control failures is considered. The solution is written in an analytical form, which makes it possible to synthesize simplified circuit implementations and adjust coefficients of the fault-tolerant control system in the case of a non-stationary object. А nonlinear medium-range aircraft model was used to verify the results.

Publisher

Vilnius Gediminas Technical University

Subject

Aerospace Engineering

Reference14 articles.

1. ACTIVE METHODS OF INCREASING RELIABILITY OF FBW CONTROL SYSTEMS FOR SMALL AIRCRAFT

2. CONTROLLERS FOR FAULT TOLERANT ACTUATORS

3. Fault Diagnosis and Reconfiguration in Flight Control Systems

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