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    SYSTEM AND A METHOD FOR FACILITATING TESTING OF PLURALITY OF DEVICES USING A DRONE
    121.
    发明申请
    SYSTEM AND A METHOD FOR FACILITATING TESTING OF PLURALITY OF DEVICES USING A DRONE 有权
    系统和方法，用于利用刮刀来提高设备的多样性测试

    公开(公告)号：US20160350593A1

    公开(公告)日：2016-12-01

    申请号：US14830987

    申请日：2015-08-20

    Applicant: HCL Technologies Ltd.

    Inventor： Siva Sakthivel SADASIVAM ,  Murali Krishnaan G ,  Vishal CHAUDHARY

    IPC: G06K9/00 ,  B64C39/02

    CPC classification number: G06K9/00536 ,  B64C39/024 ,  B64C2201/027 ,  B64C2201/042 ,  B64C2201/06 ,  B64C2201/066 ,  B64C2201/123 ,  B64C2201/126 ,  B64C2201/141 ,  B64C2201/146 ,  B64C2201/148 ,  G06K9/627 ,  G06K2209/19

    Abstract: Disclosed is a system and method for facilitating testing of a plurality of devices using a drone. At first, a locating module locates position of the drone relative to the plurality of devices. Further, a receiving module receives an image, of a device of the plurality of devices, from image capturing unit of the drone. Then, a comparing module compares the image with a reference image corresponding to the device. Based on the comparison, a determining module determines an action to be performed for testing the device. Further, a facilitating module facilitates the testing by enabling a snout associated with the drone to perform the action on the device.

    Abstract translation: 公开了一种用于促进使用无人机测试多个设备的系统和方法。 首先，定位模块相对于多个装置定位无人机的位置。 此外，接收模块从无人机的图像捕获单元接收多个设备中的设备的图像。 然后，比较模块将图像与对应于该装置的参考图像进行比较。 基于比较，确定模块确定要对设备进行测试的动作。 此外，便利模块通过启用与无人机相关联的管口来执行在该设备上的动作来促进测试。

    SYSTEM AND METHOD FOR OPERATION AND MANAGEMENT OF RECONFIGURABLE UNMANNED AIRCRAFT
    122.
    发明申请
    SYSTEM AND METHOD FOR OPERATION AND MANAGEMENT OF RECONFIGURABLE UNMANNED AIRCRAFT 有权
    可重新配置的无人驾驶飞机的运行和管理系统和方法

    公开(公告)号：US20160304199A1

    公开(公告)日：2016-10-20

    申请号：US14560765

    申请日：2014-12-04

    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 ,  THOMAS ALLAN WEAVER ,  LOWELL L. WOOD, JR.

    IPC: B64C39/02 ,  B64D47/08 ,  B64D27/26 ,  B64C27/08 ,  B64C27/52

    CPC classification number: B64C39/024 ,  B64C27/08 ,  B64C27/52 ,  B64C2201/027 ,  B64C2201/042 ,  B64C2201/044 ,  B64C2201/108 ,  B64C2201/126 ,  B64C2201/128 ,  B64D27/26 ,  B64D47/08

    Abstract: A reconfigurable unmanned aircraft system is disclosed. A system and method for configuring a reconfigurable unmanned aircraft and system and method for operation and management of a reconfigurable unmanned aircraft in an airspace are also disclosed. The aircraft is selectively reconfigurable to modify flight characteristics. The aircraft comprises a set of rotors. The position of at least one rotor relative to the base can be modified by at least one of translation of the rotor relative to the boom, pivoting of the boom relative to the base, and translation of the boom relative to the base; so that flight characteristics can be modified by configuration of position of at least one rotor relative to the base. A method of configuring an aircraft having a set of rotors on a mission to carry a payload comprises the steps of determining properties of the payload including at least mass properties, determining the manner in which the payload will be coupled to the aircraft, determining configuration for each of the rotors in the set of rotors at least partially in consideration of the properties of the payload, and positioning the set of rotors in the configuration for the aircraft to perform the mission.

    Abstract translation: 公开了一种可重新配置的无人机系统。 还公开了一种用于配置可重新配置的无人驾驶飞行器的系统和方法，以及用于在空域中操作和管理可重新配置的无人飞行器的系统和方法。 该飞机是有选择地可重构的，以修改飞行特性。 飞机包括一组转子。 相对于基座的至少一个转子的位置可以通过转子相对于起重臂的平移，悬臂相对于基座的枢转以及起重臂相对于基座的平移的至少一个来改变。 使得可以通过至少一个转子相对于基座的位置的配置来修改飞行特性。 一种在任务上配置具有一组转子的承载有效载荷的飞行器的方法包括以下步骤：确定所述载荷的属性至少包括质量属性，确定所述有效载荷将与飞行器耦合的方式，确定 转子组中的每个转子至少部分地考虑有效载荷的属性，并将该组转子定位在飞行器的构型中以执行任务。

    System and method for controlling flight operations of an unmanned aerial vehicle
    123.
    发明授权
    System and method for controlling flight operations of an unmanned aerial vehicle 有权
    用于控制无人机的飞行操作的系统和方法

    公开(公告)号：US09454157B1

    公开(公告)日：2016-09-27

    申请号：US14616663

    申请日：2015-02-07

    Applicant: Usman Hafeez ,  David Mauer

    Inventor： Usman Hafeez ,  David Mauer

    IPC: G05D1/00 ,  G05D1/10 ,  G08G5/00

    CPC classification number: G05D1/104 ,  B64C39/024 ,  B64C2201/126 ,  B64C2201/128 ,  B64C2201/14 ,  G08G5/0026 ,  G08G5/0039 ,  G08G5/0056 ,  G08G5/0069

    Abstract: The invention is directed toward a system and method for assigning mission directives to one or more unmanned vehicles and transferring mission directives from one unmanned aerial vehicle to a second unmanned aerial vehicle. The method comprises providing a set of instructions to a first unmanned aerial vehicle, storing the set of instructions on a nonvolatile memory component of the first unmanned aerial vehicle, executing one or more tasks of the set of instructions by the first unmanned aerial vehicle, transferring a set of instructions comprising unexecuted tasks from the first unmanned aerial vehicle to a second unmanned aerial vehicle, and storing the set of instructions on a nonvolatile memory component of the second unmanned aerial vehicle. The invention is further directed toward a method of determining a flight path for one or more unmanned aerial vehicles stationed at charging stations.

    Abstract translation: 本发明涉及一种用于将任务指令分配给一个或多个无人驾驶车辆并将任务指令从一个无人驾驶飞行器传送到第二无人机的系统和方法。 该方法包括向第一无人驾驶飞行器提供一组指令，将指令集存储在第一无人驾驶飞行器的非易失性存储器部件上，由第一无人驾驶飞行器执行该组指令中的一个或多个任务，传送 一组指令，其包括从第一无人飞行器到第二无人机的未执行任务，以及将该组指令存储在第二无人飞行器的非易失性存储器部件上。 本发明进一步涉及一种确定驻扎在充电站的一个或多个无人驾驶飞行器的飞行路径的方法。

    Mobile antenna array
    125.
    发明授权
    Mobile antenna array 有权
    移动天线阵列

    公开(公告)号：US09415869B1

    公开(公告)日：2016-08-16

    申请号：US14670279

    申请日：2015-03-26

    Applicant: Amazon Technologies, Inc.

    Inventor： Danny Chan ,  Eswarappa Channabasappa ,  Namhoon Kim ,  Tzung-I (Ian) Lee ,  Ulf Jan Ove Mattsson ,  Joseph Christopher Modro ,  Ming Zheng

    IPC: B64C39/02 ,  G05D1/10 ,  G08G5/00 ,  G01S5/00

    CPC classification number: B64C39/024 ,  B64C2201/027 ,  B64C2201/122 ,  B64C2201/126 ,  B64C2201/143 ,  G05D1/104 ,  G08G5/0052 ,  G08G5/0069

    Abstract: A plurality of UAVs may be operated in a fleet, each of the UAVs in the fleet being configured to work collectively to achieve one or more functions, such as to create a display or implement an antenna array. The fleet of UAVs may operate individually and/or may be coupled to one another to operate as a collective unit. In some embodiments, one or more UAVs in the fleet may operate individually, while two or more UAVs in the fleet may be connected to one another. In such embodiments, the individual UAVs and the connected UAVs may together comprise the fleet.

    Abstract translation: 多个UAV可以在车队中操作，车队中的每个UAV被配置为共同工作以实现一个或多个功能，例如创建显示器或实现天线阵列。 无人机的舰队可以单独操作和/或可以彼此耦合以作为集体单元操作。 在一些实施例中，车队中的一个或多个UAV可以单独操作，而车队中的两个或更多UAV可以彼此连接。 在这样的实施例中，各个UAV和连接的无人机可以在一起构成车队。

    DISTRIBUTED UNMANNED AERIAL VEHICLE ARCHITECTURE
    127.
    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

    Applicant: Unmanned Innovation, Inc.

    Inventor： Jonathan Downey ,  Bernard J. Michini ,  Brian Richman

    IPC: B64C39/02 ,  B64D41/00

    CPC classification number: H04L47/25 ,  B64C39/024 ,  B64C2201/126 ,  B64C2201/127 ,  B64C2201/128 ,  B64C2201/145 ,  B64D41/00 ,  B64D47/00 ,  B64D47/08 ,  G01C23/00 ,  G05D1/0022

    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。

    Airborne fulfillment center utilizing unmanned aerial vehicles for item delivery
    128.
    发明授权
    Airborne fulfillment center utilizing unmanned aerial vehicles for item delivery 有权
    机载实现中心利用无人驾驶飞行器进行货物交付

    公开(公告)号：US09305280B1

    公开(公告)日：2016-04-05

    申请号：US14580046

    申请日：2014-12-22

    Applicant: Amazon Technologies, Inc.

    Inventor： Paul William Berg ,  Scott Isaacs ,  Kelsey Lynn Blodgett

    IPC: G05D1/00 ,  G06Q10/08 ,  B64C29/00 ,  B64C39/02 ,  G05D1/10 ,  B64D5/00

    CPC classification number: G06Q10/083 ,  B64B1/00 ,  B64C39/024 ,  B64C2201/021 ,  B64C2201/022 ,  B64C2201/027 ,  B64C2201/104 ,  B64C2201/108 ,  B64C2201/126 ,  B64C2201/128 ,  B64C2201/14 ,  B64D1/08 ,  B64D5/00 ,  G05D1/104 ,  G06Q30/0265 ,  G08G5/0069

    Abstract: Described is an airborne fulfillment center (“AFC”) and the use of unmanned aerial vehicles (“UAV”) to deliver items from the AFC to users. For example, the AFC may be an airship that remains at a high altitude (e.g., 45,000 feet) and UAVs with ordered items may be deployed from the AFC to deliver ordered items to user designated delivery locations. As the UAVs descend, they can navigate horizontally toward a user specified delivery location using little to no power, other than to stabilize the UAV and/or guide the direction of descent. Shuttles (smaller airships) may be used to replenish the AFC with inventory, UAVs, supplies, fuel, etc. Likewise, the shuttles may be utilized to transport workers to and from the AFC.

    Abstract translation: 描述的是机载实现中心（“AFC”）和使用无人驾驶飞行器（“无人机”）将物品从AFC运送给用户。 例如，AFC可以是保持在高空（例如，45,000英尺）的飞艇，并且可以从AFC部署具有有序物品的UAV以将订购的物品运送到用户指定的运送地点。 随着无人机的下降，除了稳定UAV和/或引导下降方向以外，它们可以使用少量甚至无功率的水平朝向用户指定的传送位置进行导航。 可以使用班车（较小的飞艇）向库存，无人机，供应品，燃料等补充AFC。同样，梭子也可用于运输工人往返于AFC。

    Multi-Role Aircraft With Interchangeable Mission Modules
    129.
    发明申请
    Multi-Role Aircraft With Interchangeable Mission Modules 审中-公开
    具有可互换任务模块的多角色飞机

    公开(公告)号：US20160075423A1

    公开(公告)日：2016-03-17

    申请号：US14951358

    申请日：2015-11-24

    Applicant: Abe Karem

    Inventor： Abe Karem

    IPC: B64C1/00 ,  B64C25/10 ,  B64C39/10 ,  B64C3/56 ,  B64C1/06

    CPC classification number: B64C39/10 ,  B64C1/00 ,  B64C1/0009 ,  B64C1/061 ,  B64C1/065 ,  B64C1/26 ,  B64C3/56 ,  B64C25/10 ,  B64C39/024 ,  B64C2001/0072 ,  B64C2039/105 ,  B64C2201/028 ,  B64C2201/126 ,  B64C2211/00 ,  B64D37/00 ,  Y02T50/12 ,  Y02T50/14 ,  Y02T50/43

    Abstract: A flight-operable, truly modular aircraft has an aircraft core to which one or more of outer wings members, fuselage, cockpit, leading and trailing edge couplings, and empennage and tail sections can be removably coupled and/or replaced during the operating life span of the aircraft. In preferred embodiments the aircraft core houses the propulsive engines, avionics, at least 80% of the fuel, and all of the landing gear. The aircraft core is preferably constructed with curved forward and aft composite spars, that transfer loads across the center section, while accommodating a mid-wing configuration. The aircraft core preferably has a large central cavity dimensioned to interchangeably carry an ordnance launcher, a surveillance payload, electronic countermeasures, and other types of cargo. Contemplated aircraft can be quite large, for example having a wing span of at least 80 ft.

    Abstract translation: 飞行可操作的，真正模块化的飞机具有飞行器核心，一个或多个外翼构件，机身，驾驶舱，前后联轴器，尾翼和尾翼部分可在其运行寿命期间可拆卸地联接和/或更换 的飞机。 在优选实施例中，飞机核心容纳推进发动机，航空电子设备，至少80％的燃料和所有起落架。 飞机核心优选地构造有弯曲的前向和后部复合翼梁，其在中心部分处传递载荷，同时容纳中翼构造。 飞机核心优选地具有大的中心空间，其大小可互换地携带军械发射器，监视有效载荷，电子对抗措施和其他类型的货物。 考虑的飞机可能相当大，例如具有至少80英尺的翼展。

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