ISSN 0021-3454 (print version)
ISSN 2500-0381 (online version)
Menu

2
Issue
vol 67 / February, 2024
Article
UDC 519.7

ADAPTIVE CONTROL OVER LATERAL MOVEMENT OF AIRCRAFT IN THE LANDING MODE

I. B. Furtat
Institute of Problems of Mechanical Engineering, Russian Academy of Sciences, Saint Petersburg, 199178, Russian Federation; ITMO University, Saint Petersburg, 197101, Russian Federation; Leading scientific researcher professor


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


Read the full article 

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