Reconfigurable Flight Control System for Fighter Aircraft Using MPC: Fault Tolerant Flight Control Design for Aircraft Utilizing Robustness Characteristics of Model Predictive Control - Softcover
Synopsis
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.
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About the Author
Bilal A. Siddiqui received Bachelors degree in Mechanical Engineering from NED Universtiy, Pakistan in 2004. He then worked for the national space agency of Pakistan, SUPARCO as an aerodynamics and flight control systems designer. He went on to earn a Masters degree in Aerospace Engineering from KFUPM, Saudi Arabia in 2010.
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Reconfigurable Flight Control System for Fighter Aircraft Using MPC
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Reconfigurable Flight Control System for Fighter Aircraft Using MPC Fault Tolerant Flight Control Design for Aircraft Utilizing Robustness Characteristics of Model Predictive Control
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Reconfigurable Flight Control System for Fighter Aircraft Using MPC
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Taschenbuch. Condition: 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. Seller Inventory # 9783847331230
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Reconfigurable Flight Control System for Fighter Aircraft Using MPC | Fault Tolerant Flight Control Design for Aircraft Utilizing Robustness Characteristics of Model Predictive Control
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Taschenbuch. Condition: 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. Seller Inventory # 106662747
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Reconfigurable Flight Control System for Fighter Aircraft Using MPC
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Taschenbuch. Condition: 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.VDM Verlag, Dudweiler Landstraße 99, 66123 Saarbrücken 244 pp. Englisch. Seller Inventory # 9783847331230
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Reconfigurable Flight Control System for Fighter Aircraft Using MPC : Fault Tolerant Flight Control Design for Aircraft Utilizing Robustness Characteristics of Model Predictive Control
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Taschenbuch. Condition: 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. Seller Inventory # 9783847331230
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