The invention relates to a control surface jamming flight test method and system for an aircraft. The method comprises the following steps: receiving a control surface jamming flight test instruction, wherein the control surface jamming flight test instruction comprises one or more working conditions needing flight test; aiming at each specific working condition in one or more working conditions included in the control surface jamming flight test instruction, automatically carrying out flight test; and after the test flight is completed, the normal flight control system state is recovered.

    本公开涉及一种用于飞行器的舵面卡阻试飞方法和系统。该方法包括:接收舵面卡阻试飞指令,所述舵面卡阻试飞指令包括需要试飞的一个或多个工况;针对所述舵面卡阻试飞指令所包括的一个或多个工况中的每一特定工况自动进行试飞;以及:在试飞完成后恢复正常飞控系统状态。


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    Title :

    Control surface jamming flight test method and system for aircraft


    Additional title:

    用于飞行器的舵面卡阻试飞方法及系统


    Contributors:
    WEI QIANG (author) / LIU XINGHUA (author) / WU ZHIQI (author)

    Publication date :

    2023-03-07


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen



    Control surface jamming device for aircraft and control surface jamming test method and system

    WU ZHIQI / WANG XIAOHUI / WU YUZHEN et al. | European Patent Office | 2023

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