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OPTIMAL OBSERVER-BASED CONTROL DESIGN FOR AIRCRAFT LATERAL MOTION

Репозитарій Національного Авіаційного Університету

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Title OPTIMAL OBSERVER-BASED CONTROL DESIGN FOR AIRCRAFT LATERAL MOTION
 
Creator Komnatska M.M., Kiliian I. V Berezanskyi Y. A.
 
Subject aircraft lateral motion
 
Description The paper presents an alternative approach of observer-based flight control system
design. This approach is based on the application of linear matrix inequality technique.
The design procedure treats the design of both observer and controller by solving the set
of linear inequalities simultaneously. The proposed approach is free of observer poles
placement location. Simulation results demonstrate the validity and effectiveness of the
proposed design approach
 
Date 2017-07-04T09:03:32Z
2017-07-04T09:03:32Z
2015-10-08
 
Type Article
 
Identifier http://er.nau.edu.ua/handle/NAU/29961
629.735.051'622 (045)
 
Language en
 
Relation Проблеми інформатизації та управління;3(51)’2015
 
Format application/pdf
 
Publisher Національний авіаційний університет
 

Технічна підтримка: НДІІТТ НАУ