The invention discloses a test flight profile design method for premature descent alarm (PDA) function flight verification. The test flight profile design method comprises the following steps: dividing an airport surrounding area into a plurality of areas according to PDA alarm logic envelope; determining a terrain and an obstacle condition of each of the plurality of areas; determining the complexity of each region based on the terrain and obstacle conditions of each region; determining a test flight profile based on the complexity of each region; and performing test flight by adopting the determined test flight profile to verify the PDA function. The invention also discloses a test flight profile design system and a computer medium for PDA function flight verification.

    本发明公开了一种用于过早下降告警(PDA)功能飞行验证的试飞剖面设计方法,包括:根据PDA告警逻辑包络将机场周围区域划分成多个区域;确定该多个区域中每个区域的地形和障碍物状况;基于每个区域的地形和障碍物状况来确定各区域的复杂度;基于每个区域的复杂度来确定试飞剖面;以及采用所确定的试飞剖面进行试飞以验证PDA功能。还公开了用于PDA功能飞行验证的试飞剖面设计系统和计算机介质。


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    Title :

    Test flight profile design method and system for premature descent alarm (PDA) function flight verification


    Additional title:

    用于过早下降告警(PDA)功能飞行验证的试飞剖面设计方法和系统


    Contributors:
    LIU KE (author) / WU GUANGBO (author) / SU YI (author) / XU XIN (author) / LI HONGWEI (author) / ZHANG DAWEI (author) / SHEN LIXIN (author) / YU LEI (author) / LIU PENG (author)

    Publication date :

    2024-08-02


    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 / G06F ELECTRIC DIGITAL DATA PROCESSING , Elektrische digitale Datenverarbeitung



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