ABSTRACT

A model of using nonlinear control laws in the aircraft stabilization system is presented. A nonlinear control law is a device consisting of two linear algorithms and a switching device. Depending on the parameters of the control process that occurs in the stabilization system, one of the two linear control laws is selected from the condition of increasing the speed of the aircraft stabilization system. The considered system is a representative of systems with a variable structure and their use opens up wider possibilities.
Keywords: nonlinear control law, switching device, speed, stabilization system.

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