Editore: VDM Verlag Dr. Mueller Aktiengesellschaft & Co. KG, 2014
ISBN 10: 365955460X ISBN 13: 9783659554605
Lingua: Inglese
Da: Books Puddle, New York, NY, U.S.A.
EUR 45,74
Convertire valutaQuantità: 4 disponibili
Aggiungi al carrelloCondizione: New. pp. 96.
Editore: LAP LAMBERT Academic Publishing Jun 2014, 2014
ISBN 10: 365955460X ISBN 13: 9783659554605
Lingua: Inglese
Da: buchversandmimpf2000, Emtmannsberg, BAYE, Germania
EUR 32,90
Convertire valutaQuantità: 2 disponibili
Aggiungi al carrelloTaschenbuch. Condizione: Neu. Neuware -In this book, using a theoretical perspective, a design procedure is developed, to consider an innovative blend of integral sliding mode (ISM) control and control allocation (CA). An advantage of using this technique is that the structure of the ISM controller does not need to be altered during faults and failures. Maximum level of robustness of any safety critical systems can be achieved using this scheme and to make it fault tolerant. The efficiency of the proposed scheme is checked in simulation on the Admire Benchmark Model which is small rigid fighter aircraft with a delta canard configuration.Books on Demand GmbH, Überseering 33, 22297 Hamburg 96 pp. Englisch.
Editore: VDM Verlag Dr. Mueller Aktiengesellschaft & Co. KG, 2014
ISBN 10: 365955460X ISBN 13: 9783659554605
Lingua: Inglese
Da: Majestic Books, Hounslow, Regno Unito
EUR 45,49
Convertire valutaQuantità: 4 disponibili
Aggiungi al carrelloCondizione: New. Print on Demand pp. 96 2:B&W 6 x 9 in or 229 x 152 mm Perfect Bound on Creme w/Gloss Lam.
Editore: LAP LAMBERT Academic Publishing Jun 2014, 2014
ISBN 10: 365955460X ISBN 13: 9783659554605
Lingua: Inglese
Da: BuchWeltWeit Ludwig Meier e.K., Bergisch Gladbach, Germania
EUR 32,90
Convertire valutaQuantità: 2 disponibili
Aggiungi al carrelloTaschenbuch. Condizione: Neu. This item is printed on demand - it takes 3-4 days longer - Neuware -In this book, using a theoretical perspective, a design procedure is developed, to consider an innovative blend of integral sliding mode (ISM) control and control allocation (CA). An advantage of using this technique is that the structure of the ISM controller does not need to be altered during faults and failures. Maximum level of robustness of any safety critical systems can be achieved using this scheme and to make it fault tolerant. The efficiency of the proposed scheme is checked in simulation on the Admire Benchmark Model which is small rigid fighter aircraft with a delta canard configuration. 96 pp. Englisch.
Editore: VDM Verlag Dr. Mueller Aktiengesellschaft & Co. KG, 2014
ISBN 10: 365955460X ISBN 13: 9783659554605
Lingua: Inglese
Da: Biblios, Frankfurt am main, HESSE, Germania
EUR 47,86
Convertire valutaQuantità: 4 disponibili
Aggiungi al carrelloCondizione: New. PRINT ON DEMAND pp. 96.
Editore: LAP LAMBERT Academic Publishing, 2014
ISBN 10: 365955460X ISBN 13: 9783659554605
Lingua: Inglese
Da: moluna, Greven, Germania
EUR 29,02
Convertire valutaQuantità: Più di 20 disponibili
Aggiungi al carrelloCondizione: New. Dieser Artikel ist ein Print on Demand Artikel und wird nach Ihrer Bestellung fuer Sie gedruckt. Autor/Autorin: Tahir RajaasRajaas Tahir is an Electrical Engineer from Comsats Institute of Information Technology, Lahore, Pakistan. He presented publications during his graduation, in convention and as a journal paper. He is also a good athlete a.
Editore: LAP LAMBERT Academic Publishing, 2014
ISBN 10: 365955460X ISBN 13: 9783659554605
Lingua: Inglese
Da: AHA-BUCH GmbH, Einbeck, Germania
EUR 32,90
Convertire valutaQuantità: 1 disponibili
Aggiungi al carrelloTaschenbuch. Condizione: Neu. nach der Bestellung gedruckt Neuware - Printed after ordering - In this book, using a theoretical perspective, a design procedure is developed, to consider an innovative blend of integral sliding mode (ISM) control and control allocation (CA). An advantage of using this technique is that the structure of the ISM controller does not need to be altered during faults and failures. Maximum level of robustness of any safety critical systems can be achieved using this scheme and to make it fault tolerant. The efficiency of the proposed scheme is checked in simulation on the Admire Benchmark Model which is small rigid fighter aircraft with a delta canard configuration.