本发明提供一种应用于航空电磁测量系统的吊舱姿态实时调整方法,结合历史的第一类三维姿态数据以及第二类三维姿态数据,可以确定出用于描述吊舱的姿态信息的姿态偏离度指标以及姿态平稳度指标,基于姿态偏离度指标以及姿态平稳度指标,可以准确确定出吊舱的姿态调整策略。将姿态调整策略发送至飞行员,进而使飞行员可以确定出飞机的姿态调整策略,并对飞机的姿态进行调整,带动吊舱进行姿态调整,可以保证吊舱的姿态保持平稳,使吊舱测量得到的垂直磁场分量更准确,可以获得准确的倾子矢量。

    The invention provides a nacelle attitude real-time adjustment method applied to an aviation electromagnetic measurement system, which can determine an attitude deviation index and an attitude stability index for describing attitude information of a nacelle by combining historical first-class three-dimensional attitude data and second-class three-dimensional attitude data, and can accurately determine an attitude adjustment strategy of the nacelle based on the attitude deviation index and the attitude stability index. The attitude adjustment strategy is sent to a pilot, so that the pilot can determine the attitude adjustment strategy of the aircraft, adjust the attitude of the aircraft and drive a pod to perform attitude adjustment, so that the attitude of the pod can be kept stable, the vertical magnetic field component measured by the pod is more accurate, and an accurate tilter vector can be obtained.


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    Title :

    应用于航空电磁测量系统的吊舱姿态实时调整方法


    Publication date :

    2024-02-09


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    G01V Geophysik , GEOPHYSICS / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen