Items related to 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.
"synopsis" may belong to another edition of this title.
About the Author
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.
"About this title" may belong to another edition of this title.
- PublisherScholars' Press
- Publication date2014
- ISBN 10 3639714830
- ISBN 13 9783639714838
- BindingPaperback
- LanguageEnglish
- Number of pages264
Buy New
View this item
US$ 111.13
US$ 26.15 shipping from Germany to U.S.A.
Destination, rates & speedsSearch results for Robust nonlinear control system design for hypersonic...
Seller Image
Robust nonlinear control system design for hypersonic flight vehicles
Published by
Scholars' Press Jul 2014, 2014
ISBN 10: 3639714830
ISBN 13: 9783639714838
New
Taschenbuch
Seller: BuchWeltWeit Ludwig Meier e.K., Bergisch Gladbach, Germany
Seller rating 5 out of 5 stars
Taschenbuch. Condition: 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. Seller Inventory # 9783639714838
Quantity: 2 available
Seller Image
Robust nonlinear control system design for hypersonic flight vehicles
Print on DemandSeller: AHA-BUCH GmbH, Einbeck, Germany
Seller rating 5 out of 5 stars
Taschenbuch. Condition: 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. Seller Inventory # 9783639714838
Quantity: 1 available
Seller Image
Robust nonlinear control system design for hypersonic flight vehicles
Print on DemandSeller: moluna, Greven, Germany
Seller rating 5 out of 5 stars
Condition: 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. Seller Inventory # 4999574
Quantity: Over 20 available