Language: English
Published by VDM Verlag Dr. Müller, 2009
ISBN 10: 3639126661 ISBN 13: 9783639126662
Seller: Books Puddle, New York, NY, U.S.A.
Condition: New.
Language: English
Published by VDM Verlag Dr. Müller, 2009
ISBN 10: 3639126661 ISBN 13: 9783639126662
Seller: Mispah books, Redhill, SURRE, United Kingdom
Paperback. Condition: New. NEW. SHIPS FROM MULTIPLE LOCATIONS. book.
Language: English
Published by VDM Verlag Dr. Müller, 2009
ISBN 10: 3639126661 ISBN 13: 9783639126662
Seller: moluna, Greven, Germany
Kartoniert / Broschiert. Condition: New. Dieser Artikel ist ein Print on Demand Artikel und wird nach Ihrer Bestellung fuer Sie gedruckt. Autor/Autorin: Sadraey MohammadDr. Mohammad Sadraey is an Assistant Professor in the nEngineering School at the Daniel Webster College, Nashua, New nHampshire, USA. He received his MS in Aerospace Engineering in n1995 from RMIT, Melbourne, Australi.
Language: English
Published by VDM Verlag Dr. Müller, 2009
ISBN 10: 3639126661 ISBN 13: 9783639126662
Seller: Majestic Books, Hounslow, United Kingdom
Condition: New. Print on Demand.
Language: English
Published by VDM Verlag Dr. Müller, 2009
ISBN 10: 3639126661 ISBN 13: 9783639126662
Seller: Biblios, Frankfurt am main, HESSE, Germany
Condition: New. PRINT ON DEMAND.
Language: English
Published by VDM Verlag Dr. Müller, 2009
ISBN 10: 3639126661 ISBN 13: 9783639126662
Seller: AHA-BUCH GmbH, Einbeck, Germany
Taschenbuch. Condition: Neu. nach der Bestellung gedruckt Neuware - Printed after ordering - This book presents a comprehensive treatment of the analysis and design of the robust nonlinear controller for Unmanned Aerial Vehicle (UAV). Robustness against disturbances and model uncertainty is at the heart of control practice. Unmanned Aerial Vehicle flight control systems must be capable of delivering the required performance while handling nonlinearities and uncertainties in the vehicle model, the atmosphere, and ambient wind. These factors necessitate the development of nonlinear flight control system design methods that can handle large nonlinearities and uncertainties. This book presents the results of an exploratory study to examine robust nonlinear controller design methods for the UAV and compare this new approach with existing PID, LQR, and linear H techniques. The mission includes take-off, climb, cruise, a one and a half circle accomplished in a level turn, and a return back to its original airfield accomplished by cruising back, descending, and completing an approach and landing. Since the method must then be verified, its flight simulation will be done using MATLAB/SIMULINK.
Language: English
Published by VDM Verlag Dr. Müller, 2009
ISBN 10: 3639126661 ISBN 13: 9783639126662
Seller: Revaluation Books, Exeter, United Kingdom
Paperback. Condition: Brand New. 232 pages. 8.66x5.91x0.56 inches. This item is printed on demand.