New Methodology for Optimal Flight Control using Differential Evolution Algorithms applied on the Cessna Citation X Business Aircraft – Part 2. Validation on Aircraft Research Flight Level D Simulator

Article English OPEN
Yamina BOUGHARI; Georges GHAZI; Ruxandra Mihaela BOTEZ; Florian THEEL;
(2017)
  • Publisher: National Institute for Aerospace Research “Elie Carafoli” - INCAS
  • Journal: INCAS Bulletin (issn: 2066-8201, eissn: 2247-4528)
  • Publisher copyright policies & self-archiving
  • Related identifiers: doi: 10.13111/2066-8201.2017.9.2.4
  • Subject: Optimal Control; Heuristic Algorithm | Differential Evolution | TL1-4050 | Control Augmentation System | Stability Augmentation System | Linear Quadratic Regulator | Flight Control | Proportional Integrator Derivative Tuning | Motor vehicles. Aeronautics. Astronautics
    acm: ComputerApplications_COMPUTERSINOTHERSYSTEMS

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 Regulat... View more
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