Editore: LAP LAMBERT Academic Publishing, 2012
ISBN 10: 384733123X ISBN 13: 9783847331230
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Editore: LAP LAMBERT Academic Publishing, 2012
ISBN 10: 384733123X ISBN 13: 9783847331230
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Editore: LAP LAMBERT Academic Publishing, 2012
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Editore: VDM Verlag Dr. M�ller 2010-05-17, 2010
ISBN 10: 3639262255 ISBN 13: 9783639262254
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Editore: LAP LAMBERT Academic Publishing 2012-01-09, 2012
ISBN 10: 384733123X ISBN 13: 9783847331230
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Editore: LAP LAMBERT Academic Publishing, 2012
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Aggiungi al carrelloTaschenbuch. Condizione: Neu. Reconfigurable Flight Control System for Fighter Aircraft Using MPC | Fault Tolerant Flight Control Design for Aircraft Utilizing Robustness Characteristics of Model Predictive Control | Bilal Siddiqui | Taschenbuch | 244 S. | Englisch | 2012 | LAP LAMBERT Academic Publishing | EAN 9783847331230 | Verantwortliche Person für die EU: OmniScriptum GmbH & Co. KG, Bahnhofstr. 28, 66111 Saarbrücken, info[at]akademikerverlag[dot]de | Anbieter: preigu.
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Aggiungi al carrelloTaschenbuch. Condizione: Neu. Reconfigurable Flight Control For Fighter Aircraft Using MPC | Fault Tolerant Flight Control Design for Aircraft Utilizing Robustness Characteristics of Model Predictive Control | Bilal Siddiqui | Taschenbuch | Einband - flex.(Paperback) | Englisch | 2010 | VDM Verlag Dr. Müller | EAN 9783639262254 | Verantwortliche Person für die EU: OmniScriptum GmbH & Co. KG, Bahnhofstr. 28, 66111 Saarbrücken, info[at]akademikerverlag[dot]de | Anbieter: preigu.
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Editore: LAP LAMBERT Academic Publishing, 2012
ISBN 10: 384733123X ISBN 13: 9783847331230
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Editore: LAP LAMBERT Academic Publishing, 2012
ISBN 10: 384733123X ISBN 13: 9783847331230
Lingua: Inglese
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Editore: LAP LAMBERT Academic Publishing, 2012
ISBN 10: 384733123X ISBN 13: 9783847331230
Lingua: Inglese
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Editore: LAP LAMBERT Academic Publishing Jan 2012, 2012
ISBN 10: 384733123X ISBN 13: 9783847331230
Lingua: Inglese
Da: BuchWeltWeit Ludwig Meier e.K., Bergisch Gladbach, Germania
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Aggiungi al carrelloTaschenbuch. Condizione: Neu. This item is printed on demand - it takes 3-4 days longer - Neuware -In this work we studied Reconfigurable Flight Control Systems to achieve acceptable performance of a fighter aircraft, even in the event of wing damage to the aircraft at low speeds and high angle of attack, which is typical of many combat maneuvers. Equations of motion for the damaged aircraft were derived, which helped in building simulators. A new methodology for numerical prediction of aerodynamics of damaged aircraft was proposed and implemented. A baseline control system for undamaged aircraft was developed, and finally a reconfigurable flight control scheme was implemented to keep the aircraft flyable even after the damage. In this study we proposed a hybrid reconfigurable flight control system (RFCS) which was a fusion of active and passive techniques. We derived equations of motion for the damaged aircraft. The new approach to derivation lends insight into possible simplification in building simulators for damaged aircraft. A new methodology for better prediction of damaged aircraft aerodynamics. Fixed gain controller was found to be inadequate for controlling the damaged aircraft. For alleviating this a novel reconfigurable scheme based on MPC is evaluated. 244 pp. Englisch.
Editore: LAP LAMBERT Academic Publishing Jan 2012, 2012
ISBN 10: 384733123X ISBN 13: 9783847331230
Lingua: Inglese
Da: buchversandmimpf2000, Emtmannsberg, BAYE, Germania
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Aggiungi al carrelloTaschenbuch. Condizione: Neu. This item is printed on demand - Print on Demand Titel. Neuware -In this work we studied Reconfigurable Flight Control Systems to achieve acceptable performance of a fighter aircraft, even in the event of wing damage to the aircraft at low speeds and high angle of attack, which is typical of many combat maneuvers. Equations of motion for the damaged aircraft were derived, which helped in building simulators. A new methodology for numerical prediction of aerodynamics of damaged aircraft was proposed and implemented. A baseline control system for undamaged aircraft was developed, and finally a reconfigurable flight control scheme was implemented to keep the aircraft flyable even after the damage. In this study we proposed a hybrid reconfigurable flight control system (RFCS) which was a fusion of active and passive techniques. We derived equations of motion for the damaged aircraft. The new approach to derivation lends insight into possible simplification in building simulators for damaged aircraft. A new methodology for better prediction of damaged aircraft aerodynamics. Fixed gain controller was found to be inadequate for controlling the damaged aircraft. For alleviating this a novel reconfigurable scheme based on MPC is evaluated.Books on Demand GmbH, Überseering 33, 22297 Hamburg 244 pp. Englisch.
Editore: LAP LAMBERT Academic Publishing, 2012
ISBN 10: 384733123X ISBN 13: 9783847331230
Lingua: Inglese
Da: AHA-BUCH GmbH, Einbeck, Germania
EUR 79,00
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Aggiungi al carrelloTaschenbuch. Condizione: Neu. nach der Bestellung gedruckt Neuware - Printed after ordering - In this work we studied Reconfigurable Flight Control Systems to achieve acceptable performance of a fighter aircraft, even in the event of wing damage to the aircraft at low speeds and high angle of attack, which is typical of many combat maneuvers. Equations of motion for the damaged aircraft were derived, which helped in building simulators. A new methodology for numerical prediction of aerodynamics of damaged aircraft was proposed and implemented. A baseline control system for undamaged aircraft was developed, and finally a reconfigurable flight control scheme was implemented to keep the aircraft flyable even after the damage. In this study we proposed a hybrid reconfigurable flight control system (RFCS) which was a fusion of active and passive techniques. We derived equations of motion for the damaged aircraft. The new approach to derivation lends insight into possible simplification in building simulators for damaged aircraft. A new methodology for better prediction of damaged aircraft aerodynamics. Fixed gain controller was found to be inadequate for controlling the damaged aircraft. For alleviating this a novel reconfigurable scheme based on MPC is evaluated.
Da: AHA-BUCH GmbH, Einbeck, Germania
EUR 80,77
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Aggiungi al carrelloTaschenbuch. Condizione: Neu. nach der Bestellung gedruckt Neuware - Printed after ordering - In this work we studied Reconfigurable Flight Control Systems to achieve acceptable performance of a fighter aircraft, even in the event of wing damage to the aircraft at low speeds and high angle of attack, which is typical of many combat maneuvers. Equations of motion for the damaged aircraft were derived, which helped in building simulators. A new methodology for numerical prediction of aerodynamics of damaged aircraft was proposed and implemented. A baseline control system for undamaged aircraft was developed, and finally a reconfigurable flight control scheme was implemented to keep the aircraft flyable even after the damage. In this study we proposed a hybrid reconfigurable flight control system (RFCS) which was a fusion of active and passive techniques. We derived equations of motion for the damaged aircraft. The new approach to derivation lends insight into possible simplification in building simulators for damaged aircraft. A new methodology for better prediction of damaged aircraft aerodynamics. Fixed gain controller was found to be inadequate for controlling the damaged aircraft. For alleviating this a novel reconfigurable scheme based on MPC is evaluated.