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    SYSTEM AND METHOD FOR POWER TRANSFER TO AN UNMANNED AIRCRAFT
    73.
    发明申请
    SYSTEM AND METHOD FOR POWER TRANSFER TO AN UNMANNED AIRCRAFT 审中-公开
    用于向未经规定的飞机转移的系统和方法

    公开(公告)号：US20170015414A1

    公开(公告)日：2017-01-19

    申请号：US14799841

    申请日：2015-07-15

    Applicant: Elwha LLC

    Inventor： ALISTAIR K. CHAN ,  JESSE R. CHEATHAM, III ,  HON WAH CHIN ,  WILLIAM DAVID DUNCAN ,  RODERICK A. HYDE ,  MURIEL Y. ISHIKAWA ,  JORDIN T. KARE ,  TONY S. PAN ,  ROBERT C. PETROSKI ,  CLARENCE T. TEGREENE ,  DAVID B. TUCKERMAN ,  YAROSLAV A. URZHUMOV ,  THOMAS ALLAN WEAVER ,  LOWELL L. WOOD, JR. ,  VICTORIA Y.H. WOOD

    IPC: B64C39/02 ,  B60L5/00

    CPC classification number: B64C39/024 ,  B60L5/005 ,  B64C2201/024 ,  B64C2201/027 ,  B64C2201/042 ,  B64C2201/066 ,  B64C2201/108 ,  B64C2201/126 ,  B64D2203/00 ,  H02G1/02 ,  Y02T90/16

    Abstract: A system and method for repowering an unmanned aircraft system is disclosed. The system and method may comprise use of a utility transmission system configured to function as power system/source for UAV/aircraft and UAV/aircraft configured to interface with the power source/system. Systems and methods provide access and for administrating, managing, and monitoring access and interfacing by UAV/aircraft with the power system/source. UAV/aircraft system can be configured and operated/managed to interface with and use the power system/source (e.g. network of power lines from a utility transmission system) to enhance range and utility (e.g. for repowering and/or as a flyway or route). The system comprises an interface between the aircraft and the power source for power transfer; a monitoring system to monitor the aircraft; and an administrative/management system to manage interaction/transaction with the aircraft. The power source for power transfer may be a power line; power transfer to the aircraft may be by wireless power transfer (capacitive or inductive or optical) of an aircraft while at or operating along the power line. The aircraft may comprise a connector configured to interface with the power source/line; the power line may be configured to interface with the connector/aircraft. Data communications between the aircraft and system may be facilitated for interaction/transaction.

    Abstract translation: 公开了一种用于重新提供无人飞行器系统的系统和方法。 该系统和方法可以包括使用被配置为用作UAV /飞行器和被配置为与电源/系统接口的UAV /飞机的电力系统/源的公用事业传输系统。 系统和方法提供无人机/飞机与电力系统/来源的接入和管理，管理和监控接入和接口。 无人机/飞机系统可以被配置和操作/管理以与电力系统/源（例如来自公用设施传输系统的电力线的网络）接口并使用，以增强范围和效用（例如用于重新供电和/或作为飞行路线或路线 ）。 该系统包括飞机和电源之间的接口用于电力传输; 监控飞机的监控系统; 以及管理与飞机交互/交易的管理/管理系统。 电力传输的电源可以是电源线; 飞行器的电力传输可以通过在沿着电力线路或在其上运行的飞行器的无线电力传输（电容或电感或光学）。 飞行器可以包括被配置为与电源/线路接口的连接器; 电力线可以被配置为与连接器/飞行器接口。 飞机和系统之间的数据通信可能有助于交互/交易。

    WIDE AREA SENSING SYSTEM, IN-FLIGHT DETECTION METHOD, AND NON-TRANSITORY COMPUTER READABLE MEDIUM STORING PROGRAM OF WIDE AREA SENSING SYSTEM
    74.
    发明申请
    WIDE AREA SENSING SYSTEM, IN-FLIGHT DETECTION METHOD, AND NON-TRANSITORY COMPUTER READABLE MEDIUM STORING PROGRAM OF WIDE AREA SENSING SYSTEM 有权
    广域感测系统，飞行检测方法和非区域计算机可读介质存储方案

    公开(公告)号：US20170003690A1

    公开(公告)日：2017-01-05

    申请号：US14859974

    申请日：2015-09-21

    Applicant: Kabushiki Kaisha TOPCON

    Inventor： Atsushi Tanahashi

    IPC: G05D1/10 ,  G05D1/00 ,  B64C39/02

    CPC classification number: G05D1/102 ,  B64C13/20 ,  B64C19/00 ,  B64C27/00 ,  B64C27/26 ,  B64C27/30 ,  B64C29/0033 ,  B64C39/024 ,  B64C2201/021 ,  B64C2201/024 ,  B64C2201/123 ,  B64C2201/126 ,  B64C2201/127 ,  B64C2201/146 ,  G05D1/0011 ,  G05D1/0088

    Abstract: A wide area sensor system includes an unmanned airplane being switchable between an airplane mode for high speed flight and a VTOL mode for low speed flight, a state detection sensor provided in the unmanned airplane, the state detection sensor being driven to detect a state of a detection target, and an external control apparatus that controls flight of the unmanned airplane and driving of the state detection sensor. The external control apparatus performs high speed sensing by driving the state detection sensor while performing the high speed flight of the unmanned airplane in the airplane mode. The control apparatus performs low speed sensing by driving the state detection sensor while performing the low speed flight of the unmanned airplane in the VTOL mode.

    Abstract translation: 广域传感器系统包括可在飞行高速飞行模式和用于低速​​飞行的垂直起降模式之间切换的无人飞行器，设置在无人飞行器中的状态检测传感器，被驱动以检测状态检测传感器的状态 检测目标，以及控制无人驾驶飞行和状态检测传感器的驱动的外部控制装置。 外部控制装置通过在飞行模式下进行无人驾驶飞行器的高速飞行而驱动状态检测传感器来进行高速感测。 控制装置通过在以VTOL方式进行无人驾驶飞行器的低速飞行的同时驱动状态检测传感器来进行低速感测。

    SCHEDULING OF UNMANNED AERIAL VEHICLES FOR MISSION PERFORMANCE
    77.
    发明申请
    SCHEDULING OF UNMANNED AERIAL VEHICLES FOR MISSION PERFORMANCE 有权
    安排不间断的航空器用于履行任务

    公开(公告)号：US20160216711A1

    公开(公告)日：2016-07-28

    申请号：US14282205

    申请日：2014-05-20

    Applicant: Verizon Patent and Licensing Inc.

    Inventor： Ashok N. SRIVASTAVA ,  Douglas M. Pasko ,  Hani Batla ,  Igor Kantor ,  Gurpreet Ubhi

    IPC: G05D1/10 ,  B64C39/02 ,  B64D47/08 ,  G08G5/00

    CPC classification number: B64D47/08 ,  B64C39/024 ,  B64C2201/027 ,  B64C2201/123 ,  B64C2201/126 ,  G05D1/104 ,  G06Q10/00 ,  G08G5/0013 ,  G08G5/0026 ,  G08G5/0034 ,  G08G5/0052 ,  G08G5/006 ,  G08G5/0069 ,  G08G5/0078 ,  G08G5/0091 ,  G08G5/045

    Abstract: A device receives a request for a mission that includes traversal of a flight path from one or more first locations to a second location and performance of mission operations, and determines required capabilities and constraints for the mission based on the request. The device identifies UAVs based on the required capabilities and the constraints, and calculates a cost effective mission plan, for the identified UAVs, based on the required capabilities and the constraints. The device generates mission plan instructions, for the cost effective mission plan, that include flight path instructions for the flight path and mission instructions for the mission operations. The device provides the mission plan instructions to the identified UAVs to permit the identified UAVs to travel from the one or more first locations to the second location, via the flight path, and to perform the mission operations.

    Abstract translation: 设备接收对包括从一个或多个第一位置到第二位置的飞行路径的遍历以及执行任务操作的飞行任务的请求，并且基于该请求确定该任务所需的能力和约束。 该设备基于所需的能力和约束识别无人机，并根据所需的能力和约束，为所识别的UAV计算成本有效的任务计划。 该设备产生任务计划说明，用于具有成本效益的任务计划，其中包括飞行路线的飞行路线说明和任务操作的任务说明。 该设备向所识别的UAV提供任务计划指令，以允许所识别的UAV经由飞行路径从一个或多个第一位置行进到第二位置，并执行任务操作。

    UNMANNED AIR-GROUND VEHICLE
    79.
    发明申请
    UNMANNED AIR-GROUND VEHICLE 审中-公开
    未经规定的空地车

    公开(公告)号：US20160130000A1

    公开(公告)日：2016-05-12

    申请号：US14538466

    申请日：2014-11-11

    Applicant: Jon RIMANELLI

    Inventor： Jon RIMANELLI

    IPC: B64C39/02 ,  B62D55/10 ,  B60F5/02

    CPC classification number: B64C39/024 ,  B60F5/02 ,  B62D55/10 ,  B64C37/00 ,  B64C2201/024 ,  B64C2201/027 ,  B64C2201/066 ,  B64C2201/108 ,  B64C2201/126 ,  B64C2201/146 ,  B64C2201/20

    Abstract: An unmanned air-ground vehicle is provided. The unmanned air-ground vehicle includes a frame having a center portion connecting two substantially parallel transversely spaced apart track supports. Tracks that generally form loops are disposed about the track supports. Track drive motors are connected to the frame and configured to propel the tracks about the track supports. A plurality of propellers, each having propeller drive motors, are attached to the frame and disposed within the loops formed by the tracks. The tracks are configured to propel the vehicle in a ground mode while the propellers are configured to propel the vehicle in a flying mode.

    Abstract translation: 提供无人空中飞行的车辆。 无人驾驶的空中地面车辆包括具有连接两个基本上平行的横向间隔开的轨道支撑件的中心部分的框架。 通常形成环的轨道设置在轨道支撑件周围。 轨道驱动电机连接到框架并配置成推动围绕轨道支撑的轨道。 每个具有螺旋桨驱动电动机的多个螺旋桨被附接到框架并且设置在由轨道形成的环内。 轨道被配置成在地面模式下推进车辆，同时螺旋桨构造成以飞行模式推进车辆。

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