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    SYSTEM FOR AUTOMATIC TAKEOFF AND LANDING BY INTERCEPTION OF SMALL UAVS
    31.
    发明申请
    SYSTEM FOR AUTOMATIC TAKEOFF AND LANDING BY INTERCEPTION OF SMALL UAVS 审中-公开
    通过拦截小型无人机进行自动起飞和着陆的系统

    公开(公告)号：WO2015195175A3

    公开(公告)日：2016-02-11

    申请号：PCT/US2015022001

    申请日：2015-03-23

    Applicant: BORKO BRANDON

    Inventor： BORKO BRANDON

    IPC: B64F1/04 ,  E04H6/44

    CPC classification number: B64F1/04 ,  B64C39/024 ,  B64C2201/024 ,  B64C2201/08 ,  B64C2201/182 ,  B64C2201/201 ,  B64F1/12

    Abstract: A system for facilitating automated landing and takeoff of an autonomous or pilot controlled hovering air vehicle with a cooperative underbody at a stationary or mobile landing place and an automated storage system used in conjunction with the landing and takeoff mechanism that stores and services a plurality of UAVs is described. The system is primarily characterized in that the landing mechanism is settable with 6 axes in roll, pitch, yaw, and x, y and z and becomes aligned with and intercepts the air vehicle in flight and decelerates the vehicle with respect to vehicle's inertial limits. The air vehicle and capture mechanism are provided with a transmitter and receiver to coordinate vehicle priority and distance and angles between landing mechanism and air vehicle. The landing and takeoff system has means of tracking the position and orientation of the UAV in real time. The landing mechanism will be substantially aligned to the base of the air vehicle. With small UAVs, their lifting capacity is limited. Reducing sensing and computation requirements by having the landing plate perform the precision adjustments for the landing operation allows for increased flight time and/or payload capacity.

    Abstract translation: 一种用于促进自主着陆和起飞的自动着陆和起飞的自动着陆控制悬停飞行器，其具有在固定或移动着陆地点的协作车身，以及与着陆和起飞机构结合使用的自动存储系统，其存储和服务多个UAV 被描述。 该系统的主要特征在于，着陆机构可设置为具有卷轴，俯仰，偏航以及x，y和z的6个轴线，并且与飞行中的空中车辆对准并拦截，并使车辆相对于车辆的惯性极限减速。 机动车辆和捕获机构设置有发射器和接收器，以协调车辆优先级，着陆机构和空中车辆之间的距离和角度。 着陆和起飞系统具有实时跟踪无人机的位置和方向的手段。 着陆机构将基本上与机动车辆的底座对准。 对于小型无人机，起重能力有限。 通过使着陆板执行着陆操作的精确调整来减少感测和计算要求，可以增加飞行时间和/或有效负载能力。

    WEARABLE UNMANNED AERIAL VEHICLES, LAUNCH- CONTROLLED UNMANNED AERIAL VEHICLES, AND ASSOCIATED SYSTEMS AND METHODS
    32.
    发明申请
    WEARABLE UNMANNED AERIAL VEHICLES, LAUNCH- CONTROLLED UNMANNED AERIAL VEHICLES, AND ASSOCIATED SYSTEMS AND METHODS 审中-公开
    可佩戴的无人驾驶的机动车，无人驾驶的无人驾驶飞机和相关系统和方法

    公开(公告)号：WO2015200209A1

    公开(公告)日：2015-12-30

    申请号：PCT/US2015/036967

    申请日：2015-06-22

    Applicant: NIXIE LABS, INC.

    Inventor： KOHSTALL, Christoph

    IPC: B64C39/02 ,  B64C27/00 ,  B64C27/08 ,  B64C1/00 ,  A44C5/00 ,  A44C9/00

    CPC classification number: G05D1/101 ,  A44C25/00 ,  B64C39/024 ,  B64C39/028 ,  B64C2201/024 ,  B64C2201/027 ,  B64C2201/08 ,  B64C2201/108 ,  B64C2201/141 ,  B64C2201/20 ,  G05D1/0669 ,  G05D1/12

    Abstract: Unmanned aerial vehicles and associated systems and methods are disclosed. A representative unmanned aerial vehicle includes a wearable, flyable support structure, and a propulsion system carried by the support structure. The propulsion system can include a power source and a plurality of propellers. In particular embodiments, the support structure can include a wrist band. A computer- implemented method for operating an unmanned aerial vehicle in a representative embodiment includes detecting at least one parameter of a motion of the UAV as a user releases the UAV for flight. Based at least in part on the at least the one detected parameter, the method can further include establishing a flight path for the UAV, and directing the UAV to fly the flight path.

    Abstract translation: 公开了无人驾驶飞行器及相关系统和方法。 代表性的无人驾驶飞行器包括可佩戴的可飞行支撑结构以及由支撑结构承载的推进系统。 推进系统可以包括动力源和多个螺旋桨。 在特定实施例中，支撑结构可以包括腕带。 用于在代表性实施例中操作无人驾驶飞行器的计算机实现的方法包括当用户释放用于飞行的UAV时检测UAV的运动的至少一个参数。 至少部分地基于至少一个检测到的参数，该方法还可以包括建立无人机的飞行路径，并且指示无人机飞行飞行路径。

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