The invention discloses a cannon-launched takeoff control method for a cannon-launched unmanned aerial vehicle. The cannon-launched takeoff control method comprises sequential design of cannon-launched takeoff main wings, empennage unfolding and power starting and control strategies of all stages. The invention provides the cannon-launched takeoff control method for the cannon-launched unmanned aerial vehicle, provides an implementable scheme reference for the cannon-launched takeoff mode adopted by the unmanned aerial vehicle, can also be used as a reference for cannon-launched takeoff control of different fixed-wing unmanned aerial vehicles, and has engineering operability.
本发明公开了一种炮射无人机炮射起飞控制方法,包括炮射起飞主机翼、尾翼展开和动力启动的时序设计以及各阶段的控制策略。本发明提出了一种炮射无人机炮射起飞控制方法,为无人机采用炮射起飞方式提供了一种可实施的方案参考,本发明还可作为可作为不同固定翼无人机炮射起飞控制的参考,且具有工程可操作性。
Cannon-launched takeoff control method for cannon-launched unmanned aerial vehicle
一种炮射无人机炮射起飞控制方法
2021-03-02
Patent
Elektronische Ressource
Chinesisch
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 |
Europäisches Patentamt | 2023
|Cannon-Launched Guided Missile
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