The invention discloses a method for obtaining an aircraft load release window, and the method comprises the steps: building an aircraft load release model, a wind field model and an instantaneous launch aircraft model, carrying out the target shooting through Monte Carlo, and carrying out the calculation and statistics of CEP and average drop points at different heights; secondly, fitting is carried out on data of different heights and different directions, and longitudinal and lateral ranges are obtained; and finally, the longitudinal range and the lateral range are combined in the space, so that a proper load release window can be obtained.

    本发明公开了一种飞行器载荷投放窗口获得方法,该方法中,建立飞行器载荷投放模型、风场模型及发射瞬时飞行器模型,利用蒙特卡洛打靶,计算并统计出不同高度下的CEP与平均落点;其次通过对不同高度的不同方向的数据进行拟合,得到纵向和侧向范围;最后将纵向和侧向范围在空间内组合,即可得到适宜的载荷投放窗口。


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    Titel :

    Aircraft load release window obtaining method


    Weitere Titelangaben:

    一种飞行器载荷投放窗口获得方法


    Beteiligte:
    WANG HUI (Autor:in) / WANG BEI'ER (Autor:in) / YANG HAORUI (Autor:in) / DAI XIN (Autor:in) / GUO KEQING (Autor:in)

    Erscheinungsdatum :

    2024-02-20


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    G06F ELECTRIC DIGITAL DATA PROCESSING , Elektrische digitale Datenverarbeitung / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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