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    Unmanned aerial vehicle
    231.
    发明授权
    Unmanned aerial vehicle 失效
    无人驾驶的航空机

    公开(公告)号：US08720816B2

    公开(公告)日：2014-05-13

    申请号：US13130481

    申请日：2009-11-10

    Applicant: Geoffrey Salkeld

    Inventor： Geoffrey Salkeld

    IPC: B64C17/02 ,  B64C17/04

    CPC classification number: B64C39/024 ,  B64C17/04 ,  B64C27/10 ,  B64C2201/024 ,  B64C2201/108 ,  B64C2201/127 ,  B64C2201/141 ,  B64D47/08 ,  G05D1/0094

    Abstract: The present invention relates to an aircraft with a surveillance system characterized in that the direction of flight towards a target is achievable by shifting the center of gravity of the vehicle towards the target. The center of gravity is shifted towards the target by pointing the surveillance system at the target.

    Abstract translation: 本发明涉及一种具有监视系统的飞行器，其特征在于，通过将车辆的重心向目标转移，朝向目标的飞行方向是可实现的。 将监视系统指向目标，重心向目标移动。

    MEASURING SYSTEM FOR DETERMINING 3D COORDINATES OF AN OBJECT SURFACE
    233.
    发明申请
    MEASURING SYSTEM FOR DETERMINING 3D COORDINATES OF AN OBJECT SURFACE 有权
    用于确定物体表面三维坐标的测量系统

    公开(公告)号：US20140046589A1

    公开(公告)日：2014-02-13

    申请号：US14002657

    申请日：2012-04-13

    Applicant: Bernhard Metzler ,  Knut Siercks

    Inventor： Bernhard Metzler ,  Knut Siercks

    IPC: G01B21/04 ,  G05D1/00

    CPC classification number: G01B21/04 ,  B64C2201/123 ,  B64C2201/141 ,  G05D1/0094

    Abstract: A measuring system for determining 3D coordinates of measurement points on an object surface which has a scanning apparatus for measuring the measurement points on the object surface and for determining inner measurement point coordinates in an inner scanning coordinate system. Furthermore, a referencing arrangement for producing referencing information for referencing the inner measurement point coordinates in the outer object coordinate system and an evaluation unit for determining the 3D coordinates of the measurement points in the outer object coordinate system on the basis of the inner measurement point coordinates and the referencing information are provided such that the inner measurement point coordinates are in the form of 3D coordinates in the outer object coordinate system. The scanning apparatus is in this case carried in an unmanned, controllable, automotive air vehicle.

    Abstract translation: 一种用于确定物体表面上的测量点的3D坐标的测量系统，其具有用于测量物体表面上的测量点并用于确定内部扫描坐标系中的内部测量点坐标的扫描装置。 此外，用于产生用于参考外部对象坐标系中的内部测量点坐标的参考信息的参考装置和用于基于内部测量点坐标来确定外部对象坐标系中的测量点的3D坐标的评估单元 并且提供参考信息，使得内部测量点坐标是外部对象坐标系中的3D坐标的形式。 在这种情况下，扫描装置是携带在无人驾驶的，可控的汽车中的。

    FLIGHT STATE CONTROL DEVICE OF FLYING OBJECT
    234.
    发明申请
    FLIGHT STATE CONTROL DEVICE OF FLYING OBJECT 审中-公开
    飞行物体飞行状态控制装置

    公开(公告)号：US20130046459A1

    公开(公告)日：2013-02-21

    申请号：US13147599

    申请日：2010-04-22

    Applicant: Eiji Itakura

    Inventor： Eiji Itakura

    IPC: G08G5/04

    CPC classification number: B64D45/04 ,  B64C2201/141 ,  B64D45/0031 ,  G08G5/045

    Abstract: Prediction means predicts a collision risk of a flying object with at least an altitude, a flying speed, and an attitude as parameters. When the prediction means determines that the collision risk is high, flight state control means controls the flying speed, the attitude, and a flying path to control the flight state of the flying object. Therefore, when the collision risk is high, it is possible to control the maneuvering of the flying object to prevent collision and to reduce impact at the time of collision.

    Abstract translation: 预测手段预测具有至少高度，飞行速度和作为参数的姿态的飞行物体的碰撞风险。 当预测装置判定碰撞风险高时，飞行状态控制装置控制飞行速度，姿态和飞行路径，以控制飞行物体的飞行状态。 因此，当碰撞风险高时，可以控制飞行物体的操纵以防止碰撞并减少碰撞时的冲击。

    NAVIGATION ELECTRONIC CARD SUPPORT FOR A ROTARY WING DRONE
    236.
    发明申请
    NAVIGATION ELECTRONIC CARD SUPPORT FOR A ROTARY WING DRONE 失效
    导航电子卡支持旋转WONE DRONE

    公开(公告)号：US20120234969A1

    公开(公告)日：2012-09-20

    申请号：US13508959

    申请日：2010-10-15

    Applicant: Guillaume Savoye ,  Flavien Morra ,  Jean-Francois Vuillet

    Inventor： Guillaume Savoye ,  Flavien Morra ,  Jean-Francois Vuillet

    IPC: H05K7/14 ,  B64C27/00

    CPC classification number: H05K7/142 ,  A63H27/12 ,  B64C39/024 ,  B64C2201/027 ,  B64C2201/108 ,  B64C2201/141

    Abstract: The support (300) is intended to be fixed in a housing provided in the drone, through a mechanical interface (310) made of a material absorbing the mechanical vibrations. The mechanical interface, annular in shape, is intended to be attached to a corresponding annular shoulder provided in the housing. A fastening part (301) for fixing the support in the housing carries the mechanical interface (310), with at least one connection leg (302) supporting the navigation electronic card (320) and mounted free at one end on the fastening part. A battery (400) for the power supply of the drone is further accommodated in the support. The navigation electronic card may notably include a navigation sensor (321) such as an accelerometer, placed on the card in such a manner to be positioned at the barycenter of the drone.

    Abstract translation: 支撑件（300）旨在通过由吸收机械振动的材料制成的机械接口（310）固定在设置在无人机中的壳体中。 机械接口，环形形状，旨在附接到设置在壳体中的对应的环形肩部。 用于将支撑件固定在壳体中的紧固部件（301）承载机械接口（310），其中至少一个连接支脚（302）支撑导航电子卡片（320），并且一端自由地安装在紧固部件上。 用于无人机的电源的电池（400）还被容纳在支撑件中。 导航电子卡可以显着地包括放置在卡上的导航传感器（321），例如加速度计，其位于无人机的重心处。

    Automatic Taking-Off And Landing System
    237.
    发明申请
    Automatic Taking-Off And Landing System 有权
    自动起飞和着陆系统

    公开(公告)号：US20120078451A1

    公开(公告)日：2012-03-29

    申请号：US13238419

    申请日：2011-09-21

    Applicant: Fumio Ohtomo ,  Kazuki Osaragi ,  Tetsuji Anai ,  Hitoshi Otani

    Inventor： Fumio Ohtomo ,  Kazuki Osaragi ,  Tetsuji Anai ,  Hitoshi Otani

    IPC: G05D1/10 ,  G05D1/12

    CPC classification number: B64D45/08 ,  B64C39/024 ,  B64C2201/141 ,  B64C2201/145 ,  G01S5/16 ,  G01S19/15 ,  G01S19/51 ,  G05D1/0669 ,  G05D1/0676

    Abstract: The invention provides an automatic taking-off and landing system, comprising a flying object and a taking-off and landing target, wherein the flying object has an image pickup device 21 for taking images found in downward direction, navigation means 4, 5, 6, 8, 9, 10 and 11, and a control unit for processing images acquired by the image pickup device and for controlling the navigation means, and wherein the control unit calculates a positional relation between the taking-off and landing target and the flying object based on the image of the taking-off and landing target as acquired by the image pickup device and controls taking-off and landing operations of the flying object based on a result of the calculation.

    Abstract translation: 本发明提供了一种自动起飞和着陆系统，包括飞行物体和起飞着陆目标，其中飞行物体具有用于拍摄向下方向的图像的摄像装置21，导航装置4,5,6 ，8,9,10,11;以及控制单元，用于处理由图像拾取装置获取并用于控制导航装置的图像，并且其中控制单元计算起飞和着陆目标与飞行物体之间的位置关系 基于由图像拾取装置获取的起飞和着陆目标的图像，并且基于计算结果控制飞行对象的起飞和着陆操作。

    PROPULSION PROGNOSTICS APPARATUS AND SYSTEMS FOR UNMANNED AERIAL VEHICLES
    240.
    发明申请
    PROPULSION PROGNOSTICS APPARATUS AND SYSTEMS FOR UNMANNED AERIAL VEHICLES 有权
    无人驾驶飞机的推进预报装置和系统

    公开(公告)号：US20100286860A1

    公开(公告)日：2010-11-11

    申请号：US12268696

    申请日：2008-11-11

    Applicant: Eric Rowe ,  James Nickerson ,  David E. Ekhaguere ,  Richard E. Annati

    Inventor： Eric Rowe ,  James Nickerson ,  David E. Ekhaguere ,  Richard E. Annati

    IPC: G06F7/00

    CPC classification number: G05B23/0283 ,  B64C2201/141 ,  F05D2260/80 ,  G01M15/05 ,  G05B23/02 ,  G05B23/0205 ,  G05B23/0259 ,  G06N5/00 ,  G07C5/0808

    Abstract: Propulsion prognostics apparatus and systems for an unmanned aerial vehicle (UAV) are provided. One propulsion prognostics apparatus comprises a prognostics module configured to generate prognostics data and a power output sensor configured to be coupled to the engine system and configured to generate power output data representing an actual power output of the engine system. The propulsion prognostics apparatus further comprises a processor coupled to the prognostics module and the power output sensor. The processor is configured to receive the prognostics data and the power output data, compare the prognostics data and the power output data, and determine the airworthiness of the UAV based on the comparison. A propulsion prognostics system includes a UAV having an engine system and the above propulsion prognostics apparatus coupled to the UAV.

    Abstract translation: 提供了无人机（UAV）的推进预报装置和系统。 一个推进预测装置包括被配置为产生预测数据的预测模块和被配置为耦合到发动机系统并被配置为生成表示发动机系统的实际功率输出的功率输出数据的功率输出传感器。 推进预测装置还包括耦合到预测模块和功率输出传感器的处理器。 处理器被配置为接收预测数据和功率输出数据，比较预测数据和功率输出数据，并且基于比较来确定UAV的适航性。 推进预报系统包括具有发动机系统的UAV和耦合到UAV的上述推进预测装置。

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