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Flight Control Optimization from Design to Assessment Application on the Cessna Citation X Business Aircraft = = Optimisation de la commande de vol de la conception a l'evaluation application a l'avion d'affaire Cessna Citation X.

紀錄類型:	書目-語言資料,手稿 : Monograph/item
正題名/作者:	Flight Control Optimization from Design to Assessment Application on the Cessna Citation X Business Aircraft =/
其他題名:	Optimisation de la commande de vol de la conception a l'evaluation application a l'avion d'affaire Cessna Citation X.
其他題名:	Optimisation de la commande de vol de la conception a l'evaluation application a l'avion d'affaire Cessna Citation X
作者:	Boughari, Yamina.
面頁冊數:	1 online resource (227 pages)
附註:	Source: Dissertation Abstracts International, Volume: 78-11(E), Section: B.
Contained By:	Dissertation Abstracts International78-11B(E).
標題:	Aerospace engineering. -
電子資源:	click for full text (PQDT)
ISBN:	9780355058901

Flight Control Optimization from Design to Assessment Application on the Cessna Citation X Business Aircraft = = Optimisation de la commande de vol de la conception a l'evaluation application a l'avion d'affaire Cessna Citation X.
Boughari, Yamina.

Flight Control Optimization from Design to Assessment Application on the Cessna Citation X Business Aircraft =Optimisation de la commande de vol de la conception a l'evaluation application a l'avion d'affaire Cessna Citation X.Optimisation de la commande de vol de la conception a l'evaluation application a l'avion d'affaire Cessna Citation X - 1 online resource (227 pages)

Source: Dissertation Abstracts International, Volume: 78-11(E), Section: B.

Thesis (D.Eng.)

Includes bibliographical references

New methodologies have been developed to optimize the integration, testing and certification of flight control systems, an expensive process in the aerospace industry. This thesis investigates the stability of the Cessna Citation X aircraft without control, and then optimizes two different flight controllers from design to validation. The aircraft's model was obtained from the data provided by the Research Aircraft Flight Simulator (RAFS) of the Cessna Citation business aircraft.

Electronic reproduction.
Ann Arbor, Mich. :
ProQuest,
2018

Mode of access: World Wide Web

ISBN: 9780355058901Subjects--Topical Terms:

686400
Aerospace engineering.
Index Terms--Genre/Form:

554714
Electronic books.

Flight Control Optimization from Design to Assessment Application on the Cessna Citation X Business Aircraft = = Optimisation de la commande de vol de la conception a l'evaluation application a l'avion d'affaire Cessna Citation X.
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500 $a Source: Dissertation Abstracts International, Volume: 78-11(E), Section: B.
500 $a Adviser: Ruxandra Mihaela Botez.
502 $a Thesis (D.Eng.) $c Ecole de Technologie Superieure (Canada) $d 2017.
504 $a Includes bibliographical references
520 $a New methodologies have been developed to optimize the integration, testing and certification of flight control systems, an expensive process in the aerospace industry. This thesis investigates the stability of the Cessna Citation X aircraft without control, and then optimizes two different flight controllers from design to validation. The aircraft's model was obtained from the data provided by the Research Aircraft Flight Simulator (RAFS) of the Cessna Citation business aircraft.
520 $a To increase the stability and control of aircraft systems, optimizations of two different flight control designs were performed: 1) the Linear Quadratic Regulation and the Proportional Integral controllers were optimized using the Differential Evolution algorithm and the level 1 handling qualities as the objective function. The results were validated for the linear and nonlinear aircraft models, and some of the clearance criteria were investigated; and 2) the Hinfinity control method was applied on the stability and control augmentation systems. To minimize the time required for flight control design and its validation, an optimization of the controllers design was performed using the Differential Evolution (DE), and the Genetic algorithms (GA). The DE algorithm proved to be more efficient than the GA. New tools for visualization of the linear validation process were also developed to reduce the time required for the flight controller assessment.
520 $a Matlab software was used to validate the different optimization algorithms' results. Research platforms of the aircraft's linear and nonlinear models were developed, and compared with the results of flight tests performed on the Research Aircraft Flight Simulator.
520 $a Some of the clearance criteria of the optimized H-infinity flight controller were evaluated, including its linear stability, eigenvalues, and handling qualities criteria. Nonlinear simulations of the maneuvers criteria were also investigated during this research to assess the Cessna Citation X's flight controller clearance, and therefore, for its anticipated certification.
533 $a Electronic reproduction. $b Ann Arbor, Mich. : $c ProQuest, $d 2018
538 $a Mode of access: World Wide Web
650 4 $a Aerospace engineering. $3 686400
655 7 $a Electronic books. $2 local $3 554714
690 $a 0538
710 2 $a ProQuest Information and Learning Co. $3 1178819
710 2 $a Ecole de Technologie Superieure (Canada). $b Departement de genie de la production automatisee. $3 1179220
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