FIELD: aviation industry; aircraft braking systems. SUBSTANCE: pressure control signal in brakes is determined as difference of values one of which is proportional to integral of difference between preset and current values (with due account of relative slipping) of wheel angular decelerations and the other is first derivative of current value of wheel angular deceleration. EFFECT: improved efficiency of braking at considerable spread of wheel brake parameters. 1 dwg
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Authors
Dates
1998-04-10—Published
1996-04-16—Filed