The embodiment of the invention relates to an instrument landing system guided unmanned aerial vehicle approach verification flight method and system, and the method comprises the steps: enabling an airborne instrument landing navigation receiver on an unmanned aerial vehicle verification system to give a course and glide offset signal, and enabling the course and glide offset signal to be connected into an automatic driving system of an unmanned aerial vehicle platform; a course correction angle of the unmanned aerial vehicle is obtained by calculating a course offset signal, a track inclination angle correction amount of the unmanned aerial vehicle is obtained by calculating a glide offset signal, and the course correction angle and the track inclination angle correction amount are introduced into an unmanned aerial vehicle flight control system, so that approaching flight of the unmanned aerial vehicle tracking instrument landing system guide signal is realized.

    本发明实施例涉及一种基于仪表着陆系统引导的无人机进近校验飞行方法和系统,利用无人机校验系统上的机载仪表着陆导航接收机给出的航向和下滑偏移信号,将其接入无人机平台的自动驾驶系统,通过对航向偏移信号的计算得到无人机的航向修正角度,通过对下滑偏移信号的计算得到无人机的航迹倾角修正量,并将航向修正角和航迹倾角修正量引入无人机飞行控制系统,从而实现无人机追踪仪表着陆系统引导信号的进近飞行。


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    Title :

    Instrument landing system guidance-based approach verification flight method and system for unmanned aerial vehicle


    Additional title:

    基于仪表着陆系统引导的无人机进近校验飞行方法和系统


    Contributors:
    LI XIAOQIANG (author) / RONG YI (author)

    Publication date :

    2024-11-12


    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



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