An adaptive brake control method based on slip rate calculation

Abstract

The present application relates to the technical field of aircraft brake control, and particularly relates to an adaptive brake control method based on slip rate calculation, comprising: obtaining the anti-slip amount corresponding to each period when the brake is in an "instruction-deceleration rate" control strategy, and judging whether to enter the adaptive control strategy based on the slip rate. The method of the present application can effectively improve the adverse effects of runway environment on the brake effect of the aircraft, while taking into account the brake intention of the pilot, effectively identifies the current runway state to output appropriate brake pressure, and maximizes the brake efficiency of the brake system.

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