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AIRCRAFT ICING DETECTION, IDENTIFICATION AND RECONFIGURABLE CONTROL: KALMAN FILTERING AND NEURAL NETWORKS APPROACHES - Couverture souple

HAJIYEV, CHINGIZ; AYKAN, RAHMI; CALISKAN, FIKRET

 
9783844388749: AIRCRAFT ICING DETECTION, IDENTIFICATION AND RECONFIGURABLE CONTROL: KALMAN FILTERING AND NEURAL NETWORKS APPROACHES
Couverture souple
ISBN 10 : 3844388745 ISBN 13 : 9783844388749
Editeur : LAP LAMBERT Academic Publishing, 2011

Synopsis

This book aims at the detection and identification of airframe icing based on statistical properties of aircraft dynamics and reconfigurable control protecting aircraft from hazardous icing conditions. Icing model of aircraft is represented by five parameters for iced wing airfoils. Icing is detected by a Kalman filtering innovation approach. A neural network structure is embodied such that its inputs are the aircraft estimated measurements, and its outputs are the icing parameters. The necessary training and validation set for the neural network model of the iced aircraft are obtained from the simulations, which are performed for various icing conditions. In order to decrease noise effects on the states and to increase training performance of the neural network, the estimated states by the Kalman filter are used. A suitable neural network model of the iced aircraft is obtained by using system identification methods and learning algorithms. This trained network model is used as an application for the control of the aircraft that has lost its controllability due to icing. The method is applied to F16 military and A340 commercial aircraft models.

Les informations fournies dans la section « Synopsis » peuvent faire référence à une autre édition de ce titre.

Présentation de l'éditeur

This book aims at the detection and identification of airframe icing based on statistical properties of aircraft dynamics and reconfigurable control protecting aircraft from hazardous icing conditions. Icing model of aircraft is represented by five parameters for iced wing airfoils. Icing is detected by a Kalman filtering innovation approach. A neural network structure is embodied such that its inputs are the aircraft estimated measurements, and its outputs are the icing parameters. The necessary training and validation set for the neural network model of the iced aircraft are obtained from the simulations, which are performed for various icing conditions. In order to decrease noise effects on the states and to increase training performance of the neural network, the estimated states by the Kalman filter are used. A suitable neural network model of the iced aircraft is obtained by using system identification methods and learning algorithms. This trained network model is used as an application for the control of the aircraft that has lost its controllability due to icing. The method is applied to F16 military and A340 commercial aircraft models.

Biographie de l'auteur

Professor Chingiz Hajiyev graduated from Moscow Aviation Institute with honor diploma in 1981. He received the Ph.D. and D.Sc.(Eng.) degrees in 1987 and 1993, respectively. He is currently a Professor in Department of Aeronautics and Astronautics, Istanbul Technical University. He has more than 350 scientific publications.

Les informations fournies dans la section « A propos du livre » peuvent faire référence à une autre édition de ce titre.

Éditeur
LAP LAMBERT Academic Publishing
Date d'édition
2011
Langue
anglais
ISBN 10 
3844388745
ISBN 13 
9783844388749
Reliure
Broché
Nombre de pages
164
Coordonnées du fabricant
non disponible
Personne responsable
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