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

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

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 gai...

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Bibliographic Details
Main Authors: Yamina BOUGHARI, Georges GHAZI, Ruxandra Mihaela BOTEZ, Florian THEEL
Format: Article
Language:English
Published: National Institute for Aerospace Research “Elie Carafoli” - INCAS 2017-06-01
Series:INCAS Bulletin
Subjects:
Flight Control
Linear Quadratic Regulator
Optimal Control
Differential Evolution
Control Augmentation System
Stability Augmentation System
Proportional Integrator Derivative Tuning
Online Access:http://bulletin.incas.ro/files/boughari__ghazi__botez__theel__vol_9_iss_2_art_1.pdf

Internet

http://bulletin.incas.ro/files/boughari__ghazi__botez__theel__vol_9_iss_2_art_1.pdf

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