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method and flight management system for mathematically modeling the performance characteristics of an aircraft

机译:数学建模飞机性能特征的方法和飞行管理系统

摘要

The accuracy of flight management systems, based on mathematical prediction models calculated from aircraft specific data, are improved by adding engine sensor data to the calculations, checking sensor and pilot entered data, and comparing data measured from redundant sensors. A thrust estimate, calculated from available engine sensors, is added to the thrust-minus-drag aircraft model allowing prediction parameters to be accurately calculated even in a cruise condition. Sensor data and pilot entered data used in calculating predication parameters are checked to improve accuracy. Redundant sensor data is compared to determine the level of agreement. Redundant sensor data is also compared with a valid data range to find the sensor with the most accurate data.
机译:通过根据飞机特定数据计算出的数学预测模型,通过将发动机传感器数据添加到计算中,检查传感器和飞行员输入的数据以及比较从冗余传感器测量的数据,可以提高飞行管理系统的准确性。从可用的发动机传感器计算出的推力估算值将添加到推力-减阻飞机模型中,从而即使在巡航条件下也可以准确计算预测参数。检查用于计算预测参数的传感器数据和飞行员输入的数据,以提高准确性。比较冗余传感器数据以确定一致性级别。还将冗余传感器数据与有效数据范围进行比较,以找到具有最准确数据的传感器。

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