publication . Article . 2017

English

Ghazi Georges; Boughari Yamina; Theel Florian; Botez Ruxandra Mihaela;
Open Access English
  • Published: 08 Jun 2017 Journal: INCAS Bulletin (issn: 2066-8201, eissn: 2247-4528, Copyright policy)
  • Publisher: National Institute for Aerospace Research “Elie Carafoli” - INCAS
Abstract
In this paper the Cessna Citation X clearance criteria were evaluated for a new Flight Controller. The Flight Control Law were optimized and designed for the Cessna Citation X flight envelope by combining the Deferential Evolution algorithm, the Linear Quadratic Regulator method, and the Proportional Integral controller during a previous research presented in part 1. The optimal controllers were used to reach satisfactory aircraft’s dynamic and safe flight operations with respect to the augmentation systems’ handling qualities, and design requirements. Furthermore the number of controllers used to control the aircraft in its flight envelope was optimized using t...
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doi: 10.13111/2066-8201.2017.9.2.4
Subjects
ACM Computing Classification System: ComputerApplications_COMPUTERSINOTHERSYSTEMS
free text keywords: Flight Control, Linear Quadratic Regulator, Optimal Control; Heuristic Algorithm, Differential Evolution, Control Augmentation System, Stability Augmentation System, Proportional Integrator Derivative Tuning, Motor vehicles. Aeronautics. Astronautics, TL1-4050, Engineering, business.industry, business, Flight level, Simulation, Citation, Aerospace engineering
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