The invention relates to an electronic test device (20) for at least one avionics function to be tested, intended to be embedded in an aircraft (10), said aircraft (10) comprising at least one avionics item (15). The test device (20) is intended to be connected to the at least one avionics item (15) and comprises: an acquisition module (22) configured to acquire flight data (Dv) from the at leastone avionics item (15); and a calculation module (26) configured to calculate analog output data (Ds) from the acquired flight data (Dv) and via implementation of an avionics function to be tested, the avionics function to be tested being capable of delivering the output data (Ds) from the flight data (Dv).

    本发明涉及一种用于至少一个待测试航空电子功能的电子测试设备(20),旨在嵌入飞行器(10)中,所述飞行器(10)包括至少一个航空电子设备项目(15)。所述测试设备(20)旨在连接到所述至少一个航空电子设备项目(15),并且包括:‑获取模块(22),其配置为从所述至少一个航空电子设备项目(15)获取飞行数据(Dv);以及‑计算模块(26),其被配置为根据所获取的飞行数据(Dv)并且经由待测试航空电子功能的实现来计算模拟输出数据(Ds),所述待测试航空电子功能能够根据所述飞行数据(Dv)来递送所述输出数据(Ds)。


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    Title :

    Avionics function test apparatus, related aircraft, method and computer program


    Additional title:

    航空电子功能测试设备、相关飞行器、方法和计算机程序


    Contributors:

    Publication date :

    2020-11-03


    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



    Avionics function test system

    CHEN XI / LIU YAN / HAN PEICEN | European Patent Office | 2021

    Free access

    Aircraft Avionics (Digital Avionics Study)

    B. E. Bright / B. List / W. Sen et al. | NTIS | 1973