ROBUSTNESS OF THE AIRCRAFT LANDING CONTROL YSTEM BUILT IN THE CLASS OF SINGLE PARAMETER STRUCTURALLY STABLE MAPS

Uskenbayeva G. Beisenbi М. Shukirova A. Rzayeva L. Abdugulova Zh.
April 2022 Asian Research Publishing Network

ARPN Journal of Engineering and Applied Sciences
2022 #17 Issue 7 784 - 793 pp.

The article describes a method for investigating the robustness of an aircraft landing control system built in the form of a MIMO system.As a research apparatus, the gradient-velocity method of the Lyapunov function is used. The study assumes that wind gusts are equal to zero, the regulator is selected in the form of single-parameter structurally stable maps (“fold” catastrophe).The constructed function is investigated for stability in three stationary states. The results of numerical experiments confirm the existence of asymptotic stability of the system.

Control systems , Fold catastrophe , Lyapunov function , One-parameter structural lystablemapping , Robust stability , Stationary states , The aircraft landing process

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Department of System Analysis and Control, L.N. Gumilyov Eurasian National University, Astana, Kazakhstan

Department of System Analysis and Control

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