The invention discloses a micro unmanned aerial vehicle falling buffering air bag system which comprises an attitude recognition module, a flight control module, a communication module, a power module and protection air bags which are installed in an air brake control device. The air brake control device is installed under the unmanned aerial vehicle. There are two protection air bags, and the protection air bags are installed over and under the air brake control device respectively. The attitude recognition module is used for acquiring the falling attitude and the falling acceleration of the unmanned aerial vehicle under the control of the flight control module; the air brake control device is used for injecting air into the protection air bags when the falling acceleration cannot be corrected; the protection air bags are in the shape of a semi-hollow sphere after the gas injection operation is completed; the communication module is used for sending the falling attitude and the falling acceleration of the unmanned aerial vehicle to a detection terminal of an external link; and the power module is used for supplying power to the system. Therefore, the protection air bags are expanded to form an omnibearing buffer area of the unmanned aerial vehicle.
本发明公开了一种微小型无人机坠落缓冲气囊系统,包括:安装于气闸控制装置中的姿态识别模块、飞控模块、通信模块、电源模块及保护气囊;气闸控制装置安装于无人机的正下方;保护气囊数量分为2,分别安装于气闸控制装置的正上方及正下方;姿态识别模块,用于在飞控模块的控制下,获取无人机的下落姿态及下落加速度;气闸控制装置,用于在下落加速度无法修正时,向保护气囊注入气体;保护气囊在完成注入气体操作后的形状为半空心圆球体;通信模块,用于将无人机下落姿态及下落加速度发送至外部链接的检测终端;电源模块,用于为系统提供电源。从而使保护气囊膨胀,形成无人机全方位缓冲区域。
Micro unmanned aerial vehicle falling buffering air bag system
一种微小型无人机坠落缓冲气囊系统
2021-12-17
Patent
Electronic Resource
Chinese
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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