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Adaptive Load Compensation Algorithm Based on Signal Compensation Structure

This article is a study into hybrid flight control actuators operating under high external loads and mutual loads affecting the same actuators. It gives an analysis of a general simulation model of a control plant and an investigation of an adaptive control algorithm for load compensation in the system based on a special compensation structure taking into account the influence of nonlinearities and uncertainty of the system parameters. The article offers results of a practical research on the example of load compensation control for hybrid flight control actuator systems of civil aircraft transports.