Method for processing of a mathematical model of thrust - less frictional resistance of an aircraft, and method for mathematical modeling of the performance of an aircraft caracteru00ecsticas

摘要

Method for processing of a mathematical model of thrust - less frictional resistance of an aircraft, and method for mathematical modeling of caracteru00ecsticas performance of an aircraft.The accuracy of vu00f3o management systems based on mathematical models of prediction calculated from data specific to aircraft.It is improved by the addition of sensor data of motors to calculations, verification of sensor data and data entered by pilots, and the comparison of measured data of redundant sensors.An estimate of thrust calculated engine available sensors (20, 22)26) is added to the model of thrust - less frictional resistance of the aircraft allowing a precise calculation of the parameters of prediction even in a condition of vu00f3o cruise.The sensor data and data entered by pilots, used in the calculation of parameters of prediction are verified for accuracy improvement.Data from redundant sensors are compared to determine the level of agreement.The redundant sensor data are also compared with a range of valid data to be determined by the sensor that provides data more accurate.