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
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Creator |
Komnatska M.M., Kiliian I. V Berezanskyi Y. A.
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Subject |
aircraft lateral motion
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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 |
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Date |
2017-07-04T09:03:32Z
2017-07-04T09:03:32Z 2015-10-08 |
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Type |
Article
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Identifier |
http://er.nau.edu.ua/handle/NAU/29961
629.735.051'622 (045) |
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Language |
en
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Relation |
Проблеми інформатизації та управління;3(51)’2015
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Format |
application/pdf
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Publisher |
Національний авіаційний університет
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