The invention provides an aircraft control surface deflection angle test system and test method based on binocular image acquisition, and the aircraft control surface deflection angle test system comprises a binocular image acquisition structure, a main control computer and a target. The angle and position adjustment of the left and right image acquisition cameras as a whole in the horizontal direction and the vertical direction can be realized; according to the aircraft control surface deflection angle testing method, a shake removal correction algorithm and a dead pixel recognition algorithm are designed, so that the aircraft control surface deflection angle testing process is accurate, efficient and safe, and no damage is caused to a surface coating of an aircraft body.

    本发明提出了基于双目图像采集的飞机舵面偏角测试系统及测试方法,飞机舵面偏角测试系统,包含双目图像采集结构、主控计算机和靶标。可实现左右图像采集相机作为整体在水平方向、垂直方向上角度和位置的调节;飞机舵面偏角测试方法中设计了去抖修正算法和坏点识别算法,使得飞机舵面偏角测试过程准确、高效、安全,且不会对机体表面涂层造成损伤。


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    Title :

    Airplane control surface deflection angle test system and method based on binocular image acquisition


    Additional title:

    基于双目图像采集的飞机舵面偏角测试系统及测试方法


    Contributors:
    ZHANG LEILEI (author) / MAO SHAOJING (author) / HAN BING (author) / YANG FENG (author) / WANG XIN (author) / FAN JUNHUA (author)

    Publication date :

    2022-08-30


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    G01C Messen von Entfernungen, Höhen, Neigungen oder Richtungen , MEASURING DISTANCES, LEVELS OR BEARINGS / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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