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Abstract

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.