The invention relates to an ejection test emission control system which comprises far-end emission control equipment, front-end measurement and control equipment, aircraft control equipment, an optical fiber and a cable, wherein the optical fiber and the cable play a role in connection. The far-end emission control equipment comprises an emission control computer, a far-end emission control deviceand photoelectric conversion equipment I; the front-end measurement and control equipment comprises a front-end measurement and control device, a dual-channel direct-current voltage stabilization power supply and photoelectric conversion equipment II; the aircraft control equipment comprises a power supply and a time sequence controller; and the optical fiber and the cable are used for system communication. The ejection test emission control system has advantages of high real-time performance, high stability, good testability, good safety, a small size and a short development period, and meets a requirement of sequential control.

    本发明涉及一种弹射试验发射控制系统,包括:远端发控设备、前端测控设备、飞行器控制设备及起连接作用的光纤、电缆;所述远端发控设备包括发控计算机、远端发控装置和光电转换设备一;所述前端测控设备包括前端测控装置、双通道直流稳压电源和光电转换设备二;所述飞行器控制设备包括供电电源和时序控制器;所述光纤、电缆用于系统通讯。本发明的弹射试验发射控制系统具有高实时性、高稳定性、测试性好、安全性好、体积小、开发周期短的优点,满足时序控制要求。


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    Titel :

    Ejection test emission control system


    Weitere Titelangaben:

    一种弹射试验发射控制系统


    Beteiligte:
    SHEN HAIKUO (Autor:in) / WANG QING (Autor:in)

    Erscheinungsdatum :

    2020-08-25


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    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



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