飞行控制装置以及具有该飞行控制装置的无人机制造方法及图纸

一种飞行控制装置(20)，包括壳体(21)、主控板(22)以及电源管理单元(23)。所述主控板(22)设于所述壳体(21)中，并用于设置电子元器件。所述电源管理单元(23)设于所述壳体(21)上，并与所述主控板(22)电连接。所述惯性测量单元(24)设于所述壳体(21)中，并与所述主控板(22)电连接。所述主控板(22)、所述惯性测量单元(24)以及所述电源管理单元(23)与所述壳体固定连接形成一个整体。本发明专利技术还涉及一种具有所述飞行控制装置(20)的无人机。

Flight control device and unmanned aerial vehicle having the same

A flight control device (20) includes a housing (21), a master control panel (22), and a power management unit (23). The main control board (22) is arranged in the shell (21) and is used for setting electronic components. The power management unit (23) is arranged on the shell (21) and is electrically connected with the main control board (22). The inertial measuring unit (24) is arranged in the casing (21) and is electrically connected with the main control board (22). The main control panel (22), the inertial measurement unit (24) and the power management unit (23) are fixedly connected with the housing to form a whole. The invention also relates to an unmanned aerial vehicle having the flight control device (20).

【技术实现步骤摘要】
【国外来华专利技术】PCT国内申请，说明书已公开。

【技术保护点】
PCT国内申请，权利要求书已公开。

【技术特征摘要】
【国外来华专利技术】PCT国内申请，...

【专利技术属性】
技术研发人员：于云，唐尹，王永根，
申请(专利权)人：深圳市大疆创新科技有限公司，
类型：发明
国别省市：广东,44