The invention belongs to the technical field of aircraft driving, and particularly relates to an aircraft auxiliary driving method and system, and the aircraft auxiliary driving method comprises the steps: judging the flight stage of an aircraft according to flight parameters; judging the working state of the airborne system according to the airborne system information; according to the flight stage and the working state of the airborne system, obtaining the flight state of the aircraft; whether the aircraft control instruction meets the aircraft flight state safety requirement, the operation standard of the flight stage corresponding to the aircraft flight state and the aircraft flight state abnormity processing specification or not is judged, a corresponding auxiliary driving control instruction, a control suggestion and an alarm signal are generated according to the judgment result, and the aircraft is controlled through the auxiliary driving control instruction.

    本申请属于飞机驾驶技术领域,具体涉及一种飞机辅助驾驶方法及其系统飞机辅助驾驶方法,其中,飞机辅助驾驶方法包括:根据飞行参数判断飞机的飞行阶段;根据机载系统信息判断机载系统工作状态;根据飞行阶段、机载系统工作状态得到飞机飞行状态;判断飞机操控指令是否符合飞机飞行状态安全要求、飞机飞行状态对应飞行阶段的操作标准、飞机飞行状态异常处理规范,根据判断结果生成相应的辅助驾驶操控指令、操控建议、告警信号,以辅助驾驶操控指令对飞机进行控制。


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    Title :

    Airplane aided driving method and system


    Additional title:

    一种飞机辅助驾驶方法及其系统


    Contributors:
    ZHU YAN (author) / MA XIAO (author) / BAO YINGYI (author)

    Publication date :

    2022-04-12


    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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