The invention provides a test launch control system and method for a rocket-boosted unmanned aerial vehicle. The test launch control system comprises a navigation control system arranged on the unmanned aerial vehicle, a test launch control near-end system arranged on a test launch control cabinet and a far-end control system, and the booster rocket is connected with the test launch control near-end system through a cable. And then detecting onboard battery voltage and whole-aircraft bus voltage after the battery is connected to the grid, switching on a booster rocket ignition circuit when the onboard battery voltage, the whole-aircraft bus voltage and the onboard battery voltage are normal, and then controlling a near-end system to control the booster rocket to ignite by a far-end control system through test emission. The integrated control system is used, field arrangement is easy, convenient and rapid, it can be ensured that the unmanned aerial vehicle and the booster rocket are tested and have normal functions when the booster rocket ignition instruction is sent out, a rocket ignition circuit cannot be switched on when the unmanned aerial vehicle is subjected to self-inspection or airborne battery voltage and grid connection are abnormal, and launching failure caused by misoperation can be prevented.

    本发明提供了一种火箭助推无人机测试发射控制系统及方法。测试发射控制系统包括设置在无人机上的导航控制系统、设置在测试发射控制机柜上的测试发射控制近端系统、以及远端控制系统,助推火箭与测试发射控制近端系统通过电缆联接,在测试发射时,首先无人机进行发射前自检,然后检测机载电池电压和电池并网后全机母线电压,三者都正常时接通助推火箭点火电路,之后远端控制系统通过测试发射控制近端系统控制助推火箭点火。本发明使用集成的控制系统,现场布设简便快捷,能确保助推火箭点火指令发出时无人机与助推火箭均已完成测试且功能正常,在无人机自检或机载电池电压、并网异常时,火箭点火电路无法接通,可防止由于误操作造成的发射失败。


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    Title :

    Rocket-boosted unmanned aerial vehicle test launch control system and method


    Additional title:

    一种火箭助推无人机测试发射控制系统及方法


    Contributors:
    YIN HAOZHENG (author) / REN YAORU (author) / LIANG HONGDONG (author) / HAO HONGWEI (author) / MENG YAN (author)

    Publication date :

    2024-09-13


    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 / B64U



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