AIRCRAFT LANDING CONTROL SYSTEM BUILT IN THE CLASS OF FOLD CATASTROPHE
Uskenbayeva G. Beisenbi М. Shukirova A. Abdugulova Zh. Rzayeva L.
March 2022Asian Research Publishing Network
ARPN Journal of Engineering and Applied Sciences
2022#17Issue 6652 - 660 pp.
The article investigates the problem of ensuring the robust stability of the control system for the landing of an aircraft. The control law, presented in the form of one-parameter structurally stable mappings, makes it possible to build a control system with an extremely increased potential for robust stability, while the synthesized control system remains stable in a wide range of changes in the uncertain parameters of the object and the set parameters of the control device. In the study, when designing a landing control system for an aircraft, the restrictions imposed by the aircraft design are assumed to be permissible and constant, and their disturbing effects are not considered.
Control systems , Fold catastrophe , Lyapunov function , One-parameter structurally stable mapping , 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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