Reconfigurable Flight Control System for Fighter Aircraft Using MPC: Fault Tolerant Flight Control Design for Aircraft Utilizing Robustness Characteristics of Model Predictive Control - Tapa blanda

Siddiqui, Bilal

 
9783847331230: Reconfigurable Flight Control System for Fighter Aircraft Using MPC: Fault Tolerant Flight Control Design for Aircraft Utilizing Robustness Characteristics of Model Predictive Control
Tapa blanda
ISBN 10: 384733123X ISBN 13: 9783847331230
Editorial: LAP LAMBERT Academic Publishing, 2012

Sinopsis

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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Reseña del editor

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.

Biografía del autor

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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Editorial
LAP LAMBERT Academic Publishing
Año de publicación
2012
Idioma
Inglés
ISBN 10 
384733123X
ISBN 13 
9783847331230
Encuadernación
Tapa blanda
Número de páginas
244
Contacto del fabricante
no disponible
Persona responsable
no disponible