FIELD: aircrafts.
SUBSTANCE: invention relates to aircraft engineering, is designed to prevent the longitudinal rolling out of aircraft (AC) in conditions of landing on air strip (AS) and can be used in modern aircraft and remotely piloted unmanned aerial vehicles. Before landing, based on the information on board, determine the predicted value of the actual distance from the center of the landing zone to the end of the AS and compare it with the required distance to stop the AC, go to the second round or to a spare airfield, if the distance required for stopping the AC is greater than the actual distance, continue to land, if the distance required for the stop is less than the actual distance to the end of the strip, after landing, the coordinates of the AC on the AS are determined, measure the speeds of the driven and driving wheels of the landing gear AC, determine the relative slip of the wheels, determine the average value of the pressure in the tires of the wheels of the chassis, determine the actual value of the coefficient of traction of the wheels of the AC landing gear with the AS, specify the amount of the required distance to stop the AC on the AS and compare it with the actual, when the value of the actual distance exceeds the value of the actual distance, they formulate recommendations to the crew to reduce the amount of distance required to stop the aircraft or stop landing.
EFFECT: functionality of the method and the device is widened by informing the crew about the impossibility of landing, about the expediency of stopping landing on a slippery AS, continuing landing with allowance for the value of the real coefficient of adhesion of the tires of the wheels of AC the landing gear with AS.
2 cl, 2 dwg
