Articles liés à Robust nonlinear control system design for hypersonic...
Synopsis
Work presented in this book introduce new approaches to designing robust nonlinear controllers for a class of nonlinear uncertain systems. It integrates the conventional feedback linearization method with the robust control schemes such as minimax LQR and minimax LQG controllers in a systematic way. The main objective of this research is to apply the proposed method to the case of an air-breathing hypersonic flight vehicle (AHFV) control problem. In this work, we consider both rigid and flexible nonlinear models of a hypersonic flight vehicle and synthesized velocity and altitude nonlinear tracking controllers by using minimax LQR and minimax LQG controllers. The main reason to use minimax control theory is that it gives a systematic way to design a robust controller and also allows for time varying uncertainty.
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Présentation de l'éditeur
Work presented in this book introduce new approaches to designing robust nonlinear controllers for a class of nonlinear uncertain systems. It integrates the conventional feedback linearization method with the robust control schemes such as minimax LQR and minimax LQG controllers in a systematic way. The main objective of this research is to apply the proposed method to the case of an air-breathing hypersonic flight vehicle (AHFV) control problem. In this work, we consider both rigid and flexible nonlinear models of a hypersonic flight vehicle and synthesized velocity and altitude nonlinear tracking controllers by using minimax LQR and minimax LQG controllers. The main reason to use minimax control theory is that it gives a systematic way to design a robust controller and also allows for time varying uncertainty.
Biographie de l'auteur
Dr. Obaid Ur Rehman received the BE degree from NED Engineering University in 2000, the MSc degree in Automatic Control and System Engineering from University of Sheffield, UK in 2004 and the PhD degree in Electrical Engineering from University of New South Wales, Australia. He is currently with school of Engineering and IT at UNSW, Australia.
Les informations fournies dans la section « A propos du livre » peuvent faire référence à une autre édition de ce titre.
- ÉditeurScholars' Press
- Date d'édition2014
- ISBN 10 3639714830
- ISBN 13 9783639714838
- ReliureBroché
- Langueanglais
- Nombre de pages264
- Coordonnées du fabricantnon disponible
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Robust nonlinear control system design for hypersonic flight vehicles
Edité par
Scholars\' Press, 2014
ISBN 10 : 3639714830
ISBN 13 : 9783639714838
Neuf
Couverture souple
Vendeur : moluna, Greven, Allemagne
Évaluation du vendeur 5 sur 5 étoiles
Etat : New. Dieser Artikel ist ein Print on Demand Artikel und wird nach Ihrer Bestellung fuer Sie gedruckt. Autor/Autorin: Rehman Obaid UrDr. Obaid Ur Rehman received the BE degree from NED Engineering University in 2000, the MSc degree in Automatic Control and System Engineering from University of Sheffield, UK in 2004 and the PhD degree in Electrical E. N° de réf. du vendeur 4999574
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Robust nonlinear control system design for hypersonic flight vehicles
impression à la demandeVendeur : AHA-BUCH GmbH, Einbeck, Allemagne
Évaluation du vendeur 5 sur 5 étoiles
Taschenbuch. Etat : Neu. nach der Bestellung gedruckt Neuware - Printed after ordering - Work presented in this book introduce new approaches to designing robust nonlinear controllers for a class of nonlinear uncertain systems. It integrates the conventional feedback linearization method with the robust control schemes such as minimax LQR and minimax LQG controllers in a systematic way. The main objective of this research is to apply the proposed method to the case of an air-breathing hypersonic flight vehicle (AHFV) control problem. In this work, we consider both rigid and flexible nonlinear models of a hypersonic flight vehicle and synthesized velocity and altitude nonlinear tracking controllers by using minimax LQR and minimax LQG controllers. The main reason to use minimax control theory is that it gives a systematic way to design a robust controller and also allows for time varying uncertainty. N° de réf. du vendeur 9783639714838
Quantité disponible : 1 disponible(s)
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Robust nonlinear control system design for hypersonic flight vehicles
Edité par
Scholars' Press Jul 2014, 2014
ISBN 10 : 3639714830
ISBN 13 : 9783639714838
Neuf
Taschenbuch
Vendeur : BuchWeltWeit Ludwig Meier e.K., Bergisch Gladbach, Allemagne
Évaluation du vendeur 5 sur 5 étoiles
Taschenbuch. Etat : Neu. This item is printed on demand - it takes 3-4 days longer - Neuware -Work presented in this book introduce new approaches to designing robust nonlinear controllers for a class of nonlinear uncertain systems. It integrates the conventional feedback linearization method with the robust control schemes such as minimax LQR and minimax LQG controllers in a systematic way. The main objective of this research is to apply the proposed method to the case of an air-breathing hypersonic flight vehicle (AHFV) control problem. In this work, we consider both rigid and flexible nonlinear models of a hypersonic flight vehicle and synthesized velocity and altitude nonlinear tracking controllers by using minimax LQR and minimax LQG controllers. The main reason to use minimax control theory is that it gives a systematic way to design a robust controller and also allows for time varying uncertainty. 264 pp. Englisch. N° de réf. du vendeur 9783639714838
Quantité disponible : 2 disponible(s)