FIELD: physics.
SUBSTANCE: invention relates to a method for automatic control of aircraft braking. To implement the method, a pressure control signal is generated depending on the value of movement of the brake pedal and the current angular deceleration of the brake wheel considering its slippage, as well as taking into account the aircraft deceleration, created by the braking parachute according to a certain law.
EFFECT: higher reliability and efficiency of braking.
1 cl, 1 dwg
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RU2297932C1 |
