UNMANNED AERIAL VEHICLE MANAGEMENT
    36.
    发明申请
    UNMANNED AERIAL VEHICLE MANAGEMENT 审中-公开
    不定期的空中客车管理

    公开(公告)号:US20160364989A1

    公开(公告)日:2016-12-15

    申请号:US15183653

    申请日:2016-06-15

    Abstract: A base module may be used to receive and house one or more unmanned aerial vehicles (UAVs) via one or more cavities. The base module receives commands from a manager device and identifies a flight plan that allows a UAV to execute the received commands. The base module transfers the flight plan to the UAV and frees the UAV. Once the UAV returns, the base module once again receives it. The base module then receives sensor data from the UAV from one or more sensors onboard the UAV, and optionally receives additional information describing its flight and identifying success or failure of the flight plan. The base module transmits the sensor data and optionally the additional information to a storage medium locally or remotely accessible by the manager device.

    Abstract translation: 基座模块可以用于经由一个或多个空腔接收和容纳一个或多个无人机(UAV)。 基本模块从管理器设备接收命令,并识别允许UAV执行接收到的命令的飞行计划。 基地模块将飞行计划转移到无人机,并释放无人机。 一旦UAV返回,基本模块再次接收它。 然后,基本模块从UAV上的一个或多个传感器接收来自UAV的传感器数据,并且可选地接收描述其飞行并识别飞行计划的成功或失败的附加信息。 基本模块将传感器数据和可选的附加信息传输到本地或由管理器设备远程访问的存储介质。

    Airborne Drone Launch and Recovery Apparatus
    37.
    发明申请
    Airborne Drone Launch and Recovery Apparatus 审中-公开
    空中无人机发射和恢复装置

    公开(公告)号:US20160355261A1

    公开(公告)日:2016-12-08

    申请号:US15176250

    申请日:2016-06-08

    Abstract: An airborne drone launch and recovery apparatus for selectively launching drones located on the underside of a carrier aircraft or recovering drones following flight of the drones, the airborne launch and recovery apparatus has an extensible stinger slidable along the length of a stinger sheath between a retracted position proximal the rear portion of the carrier aircraft and an extended position in front of the carrier aircraft, and a catcher shuttle carried on the forward part of the stinger for extending into the non-turbulent air in front of the carrier aircraft when the stinger is in the extended position. The carrier shuttle includes a launch/recovery assembly for selectively either having a locked condition for the recovery guide of a drone prior to the positioning of the catcher shuttle in a selected for the launch of the drone, and having an open condition for receiving the recovery guide of a drone at the termination of the flight of the drone to terminate the flight.

    Abstract translation: 一种空中无人机发射和恢复装置,用于选择性地发射位于载体飞行器的下侧上的无人机或在无人机的飞行之后恢复无人机,机载发射和恢复装置具有可伸长的刺针,沿着刺血刺鞘的长度在缩回位置 靠近载体飞行器的后部,并且在载体飞行器的前面延伸的位置,以及在托管架前部延伸到载体飞行器前方的非湍流空气中的捕手穿梭器,当托管架处于 延长的位置。 运输班车包括发射/恢复组件,用于选择性地具有用于无人机的恢复引导件的锁定状态,在捕集器穿梭机定位在被选择用于发射无人机之前,并且具有用于接收恢复的打开状态 在无人驾驶飞机终止时终止飞行的无人机指导。

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