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。


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

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


    Weitere Titelangaben:

    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


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

    Erscheinungsdatum :

    02.08.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    G08G Anlagen zur Steuerung, Regelung oder Überwachung des Verkehrs , TRAFFIC CONTROL SYSTEMS / G06F ELECTRIC DIGITAL DATA PROCESSING , Elektrische digitale Datenverarbeitung



    Ground flight test system for hypersonic flight vehicle design verification

    LIN ZHIYONG / YAO JUNYU / QIN SHUN et al. | Europäisches Patentamt | 2024

    Freier Zugriff

    TCAS alarm verification and alarm avoidance system and method for double-runway flight

    HUANG RONGSHUN / WANG XUHUI / YANG LE et al. | Europäisches Patentamt | 2020

    Freier Zugriff


    HUYGENS Probe: Thermal Design, Test, Flight Comparison, and Descent Prediction

    Cluzet, G. / Doenecke, J. / Vollmer, K. et al. | British Library Conference Proceedings | 1998