DISTRIBUTED UNMANNED AERIAL VEHICLE ARCHITECTURE
    1.
    发明申请
    DISTRIBUTED UNMANNED AERIAL VEHICLE ARCHITECTURE 审中-公开
    分布式无人驾驶车辆结构

    公开(公告)号:US20160285774A1

    公开(公告)日:2016-09-29

    申请号:US15174387

    申请日:2016-06-06

    Abstract: Methods, systems, and apparatus, including computer programs encoded on computer storage media, for a distributed system architecture for unmanned air vehicles. One of the methods includes obtaining information identifying flight information of a UAV, with the flight information including flight phase information or a contingency condition associated with a flight critical module included in the UAV. The obtained information is analyzed, and one or more first payload modules are determined to enter a modified power state. Requests to enter the modified power state are caused to be transmitted to each determined payload module in the one or more first payload modules.

    Abstract translation: 方法,系统和装置,包括在计算机存储介质上编码的计算机程序,用于无人驾驶飞行器的分布式系统架构。 其中一种方法包括获得识别无人机的飞行信息的信息,其中飞行信息包括飞行相位信息或与包括在UAV中的飞行关键模块相关联的应急条件。 分析所获得的信息,并且确定一个或多个第一有效载荷模块进入修改的功率状态。 使得进入修改的功率状态的请求被发送到一个或多个第一有效载荷模块中的每个确定的有效载荷模块。

    Distributed unmanned aerial vehicle architecture
    4.
    发明授权
    Distributed unmanned aerial vehicle architecture 有权
    分布式无人机架构

    公开(公告)号:US09340283B1

    公开(公告)日:2016-05-17

    申请号:US14989701

    申请日:2016-01-06

    Abstract: Methods, systems, and apparatus, including computer programs encoded on computer storage media, for a distributed system architecture for unmanned air vehicles. One of the methods includes receiving selections of configuration information to provide to an unmanned aerial vehicle (UAV), with the selections of configuration information being associated with respective components included in the UAV. The configuration information associated with a first component is determined to be valid from selections of configuration information associated with the first component. The configuration information associated with the first component is provided for storage in the UAV in response to receiving a user action.

    Abstract translation: 方法,系统和装置,包括在计算机存储介质上编码的计算机程序,用于无人驾驶飞行器的分布式系统架构。 其中一种方法包括接收配置信息的选择以提供给无人驾驶飞行器(UAV),其中配置信息的选择与包括在UAV中的各个部件相关联。 通过从与第一组件相关联的配置信息的选择来确定与第一组件相关联的配置信息是有效的。 提供与第一组件相关联的配置信息以响应于接收用户动作而存储在UAV中。

    DISTRIBUTED UNMANNED AERIAL VEHICLE ARCHITECTURE
    5.
    发明申请
    DISTRIBUTED UNMANNED AERIAL VEHICLE ARCHITECTURE 有权
    分布式无人驾驶车辆结构

    公开(公告)号:US20160114888A1

    公开(公告)日:2016-04-28

    申请号:US14989701

    申请日:2016-01-06

    Abstract: Methods, systems, and apparatus, including computer programs encoded on computer storage media, for a distributed system architecture for unmanned air vehicles. One of the methods includes receiving selections of configuration information to provide to an unmanned aerial vehicle (UAV), with the selections of configuration information being associated with respective components included in the UAV. The configuration information associated with a first component is determined to be valid from selections of configuration information associated with the first component. The configuration information associated with the first component is provided for storage in the UAV in response to receiving a user action.

    Abstract translation: 方法,系统和装置,包括在计算机存储介质上编码的计算机程序,用于无人驾驶飞行器的分布式系统架构。 其中一种方法包括接收配置信息的选择以提供给无人驾驶飞行器(UAV),其中配置信息的选择与包括在UAV中的各个部件相关联。 通过从与第一组件相关联的配置信息的选择来确定与第一组件相关联的配置信息是有效的。 提供与第一组件相关联的配置信息以响应于接收用户动作而存储在UAV中。

    UNMANNED AERIAL VEHICLE AUTHORIZATION AND GEOFENCE ENVELOPE DETERMINATION

    公开(公告)号:US20170154535A1

    公开(公告)日:2017-06-01

    申请号:US15431057

    申请日:2017-02-13

    Abstract: Methods, systems, and apparatus, including computer programs encoded on computer storage media, for unmanned aerial vehicle authorization and geofence envelope determination. One of the methods includes determining, by an electronic system in an Unmanned Aerial Vehicle (UAV), an estimated fuel remaining in the UAV. An estimated fuel consumption of the UAV is determined. Estimated information associated with wind affecting the UAV is determined using information obtained from sensors included in the UAV. Estimated flights times remaining for a current path, and one or more alternative flight paths, are determined using the determined estimated fuel remaining, determined estimated fuel consumption, determined information associated wind, and information describing each flight path. In response to the electronic system determining that the estimated fuel remaining, after completion of the current flight path, would be below a first threshold, an alternative flight path is selected.

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