publication . Article . 2017

New Methodology for Optimal Flight Control Using Differential Evolution Algorithms Applied on the Cessna Citation X Business Aircraft – Part 1. Design and Optimization

Yamina BOUGHARI; Georges GHAZI; Ruxandra Mihaela BOTEZ; Florian THEEL;
Open Access English
  • Published: 01 Jun 2017 Journal: INCAS Bulletin (issn: 2066-8201, eissn: 2247-4528, Copyright policy)
  • Publisher: National Institute for Aerospace Research “Elie Carafoli” - INCAS
Setting the appropriate controllers for aircraft stability and control augmentation systems are complicated and time consuming tasks. As in the Linear Quadratic Regulator method gains are found by selecting the appropriate weights or as in the Proportional Integrator Derivative control by tuning gains. A trial and error process is usually employed for the determination of weighting matrices, which is normally a time consuming procedure. Flight Control Law were optimized and designed by combining the Deferential Evolution algorithm, the Linear Quadratic Regulator method, and the Proportional Integral controller. The optimal controllers were used to reach satisfac...
free text keywords: Flight Control, Linear Quadratic Regulator, Optimal Control, Differential Evolution, Control Augmentation System, Stability Augmentation System, Proportional Integrator Derivative Tuning, Motor vehicles. Aeronautics. Astronautics, TL1-4050
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