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Robustness of the aircraft landing control system built in the class of single parameter structurally stable MAPS

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Title: Robustness of the aircraft landing control system built in the class of single parameter structurally stable MAPS

Authors: G. Uskenbayeva, M. Beisenbi, A. Shukirova, L. Rzayeva, Zh. Abdugulova

Journal: ARPN Journal of Engineering and Applied Sciences

HEC Recognition History
Category From To
Y 2023-07-01 2024-09-30
Y 2022-07-01 2023-06-30
Y 2021-07-01 2022-06-30
X 2020-07-01 2021-06-30

Publisher: Khyber Medical College, Peshawar

Country: Pakistan

Year: 2022

Volume: 17

Issue: 7

Language: English

Categories
Aircraft Systems (4) Flight Control Systems (3) Robust Control (5) Aerospace Engineering (534) Control Engineering (432)

Abstract

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.

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