The aircraft has a first principle takeoff processor (PCE), a predictive flight envelope protection processor (PFEP), and a maximum takeoff weight processor. The PCE is programmed to predict a terrain clearance position and an energy state when the aircraft is terrain clearance on a runway. The PFEP is programmed to assess whether each of the plurality of potential trajectories conforms to or violates a predetermined flight envelope. The maximum weight processor is programmed to: indicate that the aircraft is capable of takeoff at an aircraft weight when any of the plurality of potential trajectories conforms to a predetermined flight envelope; iteratively reducing the input of aircraft weight to the PCE until the PCE indicates that any one of the plurality of potential trajectories conforms to a predetermined flight envelope; and the input indicating the reduced aircraft weight is the maximum allowable takeoff weight.

    飞行器具有第一原理起飞处理器(PCE)、预测飞行包线保护处理器(PFEP)和最大起飞重量处理器。PCE被编程为预测飞行器在跑道上离地时的离地位置和能量状态。PFEP被编程为评估多个潜在轨迹中的每一个是符合还是违反预定飞行包线。最大重量处理器被编程为:当多个潜在轨迹中的任何一个符合预定飞行包线时,指示飞行器能够在飞行器重量下起飞;迭代地减少飞行器重量向PCE的输入,直到PCE指示多个潜在轨迹中的任何一个符合预定飞行包线;以及指示减少的飞行器重量的输入是最大允许起飞重量。


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    Title :

    Maximum takeoff weight determination of aircraft


    Additional title:

    飞行器的最大起飞重量确定


    Contributors:

    Publication date :

    2025-01-14


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    G08G Anlagen zur Steuerung, Regelung oder Überwachung des Verkehrs , TRAFFIC CONTROL SYSTEMS



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