ISSN 0021-3454 (print version)
ISSN 2500-0381 (online version)
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11
Issue
vol 67 / November, 2024
Article
UDC 519.7

ADAPTIVE CONTROL OVER LATERAL MOVEMENT OF AIRCRAFT IN THE LANDING MODE

I. B. Furtat
ITMO University, Saint Petersburg, 197101, Russian Federation; Institute of Problems of Mechanical Engineering of the Russian Academy of Sciences, Saint Petersburg, 199178, Russian Federation; Full Professor; Head of Department, Chief Researcher


K. A. Khvostova
ITMO University, Department of Control Systems and Computer Science;


D. A. Khvostov
Saint Petersburg National Research University of Information Technologies, Mechanics and Optics (ITMO University), Saint Petersburg, Russia; student


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Abstract. A solution to the problem of adaptive control over lateral movement of aircraft in the landing mode is proposed. The control system with a reference model based on modified algorithm of high order adaptation is developed. Simulation results are presented to illustrate the efficiency of the synthesized algorithm.
Keywords: aircraft, adaptive control, optimal control