Authors: V. Apostolyuk, I. Dovgan
Publisher: Methods and Systems of Navigation and Motion Control, 2010, pp. 128-131
Abstract: The objective of this paper is to research the designed control system robustness to change of control object's
parameters (engine thrust, aircraft mass, shift centre of gravity, change of the wing area) as well as to define the optimal genetic algorithm’s parameters which will minimize altitude control error and time of transient process when the aircraft changes to another flight echelon.
Reference: Apostolyuk V.O., Dovgan A.I. Neural Network Based Adaptive Control System for Aircrafts // Methods and Systems of Navigation and Motion Control: 1-st international conference, 13-16 October 2010 р.: proceedings. – К.: НАУ, 2010.– С. 128-131.
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