The invention relates to the technical field of aviation safety, in particular to an aircraft bumping risk assessment and inspection method. According to the invention, flight environment data including but not limited to wind speed, wind direction, air pressure, temperature, humidity, illumination intensity and atmosphere stability are collected in real time through a plurality of sensors installed on the unmanned aerial vehicle, and the data are analyzed by using a pre-constructed mapping relation model between environmental conditions and bumping probabilities. The bumping risk level in the current flight environment is quickly and accurately evaluated, and alarm information and corresponding flight parameter adjustment suggestions are sent to an unmanned aerial vehicle control system, so that various potential safety threats caused by bumping are effectively reduced.

    本发明涉及航空安全技术领域,尤其涉及一种飞机颠簸风险评估检查方法。本发明旨在通过安装在无人机上的多种传感器实时采集包括但不限于风速、风向、气压、温度、湿度、光照强度及大气层稳定性在内的飞行环境数据,利用预先构建的环境条件与颠簸概率之间映射关系模型对这些数据进行分析,快速准确地评估出当前飞行环境下的颠簸风险等级,并据此向无人机控制系统发送警报信息及相应的飞行参数调整建议,从而有效降低因颠簸导致的各种潜在安全威胁。


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    Title :

    Aircraft bumping risk assessment and inspection method


    Additional title:

    一种飞机颠簸风险评估检查方法


    Contributors:
    XU WENWEN (author) / ZHENG YANXIN (author) / MAO XIN (author) / XU TING (author) / YANG JUN (author)

    Publication date :

    2025-05-23


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    G06N COMPUTER SYSTEMS BASED ON SPECIFIC COMPUTATIONAL MODELS , Rechnersysteme, basierend auf spezifischen Rechenmodellen / G01D MEASURING NOT SPECIALLY ADAPTED FOR A SPECIFIC VARIABLE , Anzeigen oder Aufzeichnen in Verbindung mit Messen allgemein / G07C TIME OR ATTENDANCE REGISTERS , Zeit- oder Anwesenheitskontrollgeräte / G08G Anlagen zur Steuerung, Regelung oder Überwachung des Verkehrs , TRAFFIC CONTROL SYSTEMS



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