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    REMOTE CONTROL METHOD AND TERMINAL
    113.
    发明申请
    REMOTE CONTROL METHOD AND TERMINAL 审中-公开

    公开(公告)号：US20150268666A1

    公开(公告)日：2015-09-24

    申请号：US14670107

    申请日：2015-03-26

    Applicant: SZ DJI TECHNOLOGY Co., Ltd

    Inventor： Tao Wang ,  Mingyu Wang

    IPC: G05D1/00 ,  G06F3/0488 ,  B64C39/02

    CPC classification number: G05D1/0094 ,  B64C39/024 ,  B64C2201/123 ,  B64C2201/127 ,  B64C2201/146 ,  B64D47/08 ,  G05D1/0016 ,  G05D1/0038 ,  G06F3/04883

    Abstract: The present application discloses a remote control method and apparatus for controlling the state of a movable object and/or a load carried thereon. The remote control method comprising: receiving, via an apparatus, a state signal that corresponds to a user's position; remote-controlling the state of the a load being carried on a movable object based on the state signal; wherein the state of the load is the result of combining the movement of the load relative to the movable object and the movement of the object relative to its environment. For example, the control of the state can be achieved through the state of the apparatus itself, a user's state captured by an apparatus, a graphical interface on a screen of an apparatus, or a voice command.

    SUSTAINED OVER-THE-HORIZON VERTICAL TAKEOFF AND LANDING SENSING SYSTEM
    115.
    发明申请
    SUSTAINED OVER-THE-HORIZON VERTICAL TAKEOFF AND LANDING SENSING SYSTEM 有权
    可持续发展的垂直起落架和陆地传感系统

    公开(公告)号：US20140316608A1

    公开(公告)日：2014-10-23

    申请号：US13866489

    申请日：2013-04-19

    Applicant: SIKORSKY AIRCRAFT CORPORATION

    Inventor： Mark R. Alber ,  Timothy Fred Lauder ,  Jonathan Hartman ,  Bryan Clark Holasek

    IPC: B64C19/00 ,  B64C29/00 ,  B64D47/00 ,  B64C39/02

    CPC classification number: B64C19/00 ,  B64C29/00 ,  B64C39/022 ,  B64C39/024 ,  B64C2201/024 ,  B64C2201/042 ,  B64C2201/06 ,  B64C2201/123 ,  B64C2201/148 ,  B64D47/00

    Abstract: An electrically powered of the vertical takeoff and landing aircraft configured for use with a tether station having a continuous power source is provided including at least one rotor system. The vertical takeoff and landing aircraft additionally has an autonomous flight control system coupled to the continuous power source. The autonomous flight control system is configured to operate an electrical motor coupled to the at least one rotor system such that the vertical takeoff and landing aircraft continuously hovers above the tether station in a relative position. The vertical takeoff and landing aircraft also includes a detection system for detecting objects at a distance from the vertical takeoff and landing aircraft.

    Abstract translation: 提供了一种配置成与具有连续动力源的系绳站一起使用的垂直起飞和着陆飞机的电力供应器，其包括至少一个转子系统。 垂直起飞和着陆飞机还具有耦合到连续电源的自主飞行控制系统。 自主飞行控制系统被配置为操作耦合到至少一个转子系统的电动机，使得垂直起飞和着陆飞机在相对位置连续地悬挂在系绳站上方。 垂直起降飞机还包括一个检测系统，用于检测与垂直起飞和着陆飞机相距一定距离处的物体。

    Foldable rise and stare vehicle
    116.
    发明授权
    Foldable rise and stare vehicle 有权
    可折叠上升和凝视车辆

    公开(公告)号：US08844860B2

    公开(公告)日：2014-09-30

    申请号：US13543722

    申请日：2012-07-06

    Applicant: Gert Magnus Lundgren

    Inventor： Gert Magnus Lundgren

    IPC: B64C11/00

    CPC classification number: A63H27/12 ,  B64C39/024 ,  B64C2201/027 ,  B64C2201/042 ,  B64C2201/108 ,  B64C2201/123

    Abstract: A Foldable Rise and Stare Vehicle with a single engine assembly that contains a pair of inline counter-rotating propellers. Two inline counter-rotating engines are directly connected to the propellers. Gimbal mounting the engine assembly permits thrust to be directed forward to back and left to right to control the vehicle position in the horizontal plane, when hovering. Varying the relative engine speeds controls yaw. The Foldable Rise and Stare Vehicle is adaptable as an unmanned vehicle.The vehicle collapses into a flat assembly similar to a foldable beach chair, allowing for convenient transportation.

    Abstract translation: 具有单个发动机组件的可折叠上升和怠速车辆，其包含一对在线的反向旋转螺旋桨。 两个内联反向旋转发动机直接连接到螺旋桨。 安装发动机总成的万向节可以在悬停时将推力向前指向前后左右，以控制水平面中的车辆位置。 改变相对发动机转速来控制偏航。 可折叠起升车辆适用于无人驾驶车辆。 车辆塌陷成类似于可折叠沙滩椅的平板组件，允许便利的运输。

    Hovering Surveillance Air Vehicle
    117.
    发明申请
    Hovering Surveillance Air Vehicle 审中-公开
    悬停监控机动车

    公开(公告)号：US20140284422A1

    公开(公告)日：2014-09-25

    申请号：US13848443

    申请日：2013-03-21

    Applicant: Itzhak Sapir

    Inventor： Itzhak Sapir

    IPC: B64B1/00

    CPC classification number: B64B1/24 ,  B64B1/40 ,  B64B1/62 ,  B64C2201/022 ,  B64C2201/101 ,  B64C2201/121 ,  B64C2201/123

    Abstract: A hovering surveillance device. An electronic imaging device is disposed on a housing having a primary lift element, at least one compressed lighter-than-air gas element, a pitch adjustment element, and, a steering element. The compressed lighter-than-air gas is channeled to the primary lift element and the pitch adjustment element to selectively vary the altitude and angle for the housing such that scene of interest may be imaged. The lighter-than-air gas may be selected from the group of helium, hydrogen, heated air, neon, ammonia, and methane.

    Abstract translation: 悬停监视装置。 电子成像装置设置在具有主提升元件的壳体上，至少一个压缩的轻质空气气体元件，俯仰调节元件和转向元件。 压缩的轻型空气气体被引导到主提升元件和俯仰调节元件以选择性地改变壳体的高度和角度，使得可以对感兴趣的场景进行成像。 轻于空气的气体可以选自氦气，氢气，加热空气，氖气，氨气和甲烷。

    AERIAL IMAGE COLLECTION
    118.
    发明申请
    AERIAL IMAGE COLLECTION 有权
    空中影像收藏

    公开(公告)号：US20140257595A1

    公开(公告)日：2014-09-11

    申请号：US13785796

    申请日：2013-03-05

    Applicant: NAVTEQ B.V.

    Inventor： Marco Tillmann

    IPC: B64C19/00

    CPC classification number: G05D1/0022 ,  B64C39/024 ,  B64C2201/024 ,  B64C2201/123 ,  B64C2201/146 ,  G01C11/02 ,  G01C11/06 ,  G01C11/08 ,  G05D1/0094 ,  G06T17/00

    Abstract: In one embodiment, an aerial collection system includes an image collection field vehicle that travels at street level and an image collection aerial vehicle that travels in the air above the street. The aerial vehicle collects image data including at least a portion of the field vehicle. The field vehicle includes a marker, which is identified from the collected image data. The marker is analyzed to determine an operating characteristic of the aerial vehicle. In one example, the operating characteristic in the marker includes information for a flight instruction for the aerial vehicle. In another example, the operating characteristic in the marker includes information for the three dimensional relationship between the vehicles. The three dimensional relationship is used to combine images collected from the air and images collected from the street level.

    Abstract translation: 在一个实施例中，空中收集系统包括在街道行驶的图像采集野外车辆和在街道上空中行进的图像收集空中飞行器。 飞行器收集包括现场车辆的至少一部分的图像数据。 现场车辆包括从收集的图像数据识别的标记。 分析标记以确定飞行器的操作特性。 在一个示例中，标记中的操作特征包括用于飞行器的飞行指令的信息。 在另一示例中，标记中的操作特性包括用于车辆之间的三维关系的信息。 三维关系用于组合从空中收集的图像和从街道级采集的图像。

    GEODETIC MARKING SYSTEM FOR MARKING TARGET POINTS
    119.
    发明申请
    GEODETIC MARKING SYSTEM FOR MARKING TARGET POINTS 有权
    用于标记目标点的地球标记系统

    公开(公告)号：US20140163775A1

    公开(公告)日：2014-06-12

    申请号：US14008519

    申请日：2012-04-13

    Applicant: Bernhard Metzler

    Inventor： Bernhard Metzler

    IPC: B64C19/00

    CPC classification number: B64C19/00 ,  B64C2201/123 ,  G01C15/002 ,  G01S19/07 ,  G01S19/11 ,  G01S19/51 ,  G05D1/102

    Abstract: A geodetic marking system for marking a known target point, having an automotive, unmanned, remotely controllable air vehicle and having a geodetic position determination arrangement for determining the external actual position of the air vehicle. The air vehicle also has a marking unit for marking the target point, and the marking system has a control unit such that the air vehicle can be positioned relative to the target point position on the basis of the external actual position, which can be determined continuously. The control unit is also configured in such a manner that it is possible to control the marking unit for marking the target point taking into account the actual position, the desired position and a defined marking direction from the marking unit to the target point, with the result that the target point can be marked with geodetic accuracy in the defined marking direction.

    Abstract translation: 一种用于标记已知目标点的大地测量标记系统，具有汽车，无人驾驶的可远程控制的飞行器，并具有用于确定所述空中交通工具的外部实际位置的大地测位位置确定装置。 空中客车还具有用于标记目标点的标记单元，并且标记系统具有控制单元，使得可以基于可以连续确定的外部实际位置相对于目标点位置定位空中车辆 。 控制单元还被构造成使得可以控制用于标记目标点的标记单元，其考虑到从标记单元到目标点的实际位置，期望位置和确定的标记方向，其中 导致目标点可以在定义的标记方向上以大地测量精度标记。

    REMOTE DETECTION, CONFIRMATION AND DETONATION OF BURIED IMPROVISED EXPLOSIVE DEVICES
    120.
    发明申请
    REMOTE DETECTION, CONFIRMATION AND DETONATION OF BURIED IMPROVISED EXPLOSIVE DEVICES 有权
    破坏性改进的爆炸装置的远程检测，确认和爆炸

    公开(公告)号：US20140062754A1

    公开(公告)日：2014-03-06

    申请号：US13656382

    申请日：2012-10-19

    Applicant: Farrokh Mohamadi

    Inventor： Farrokh Mohamadi

    IPC: F41H11/136 ,  B64D47/08 ,  F41H11/13 ,  B64C19/00

    CPC classification number: F41H11/136 ,  B64C19/00 ,  B64C2201/027 ,  B64C2201/123 ,  B64C2201/145 ,  B64D47/08 ,  F41H11/13 ,  F41H11/16

    Abstract: A small unmanned aerial system (sUAS) is used for remotely detecting concealed explosive devices—such as buried or otherwise hidden improvised explosive devices (IED)—and exploding or disarming the device while an operator of the sUAS, or other personnel, remain at a safe distance. The sUAS system can be operated at an extended, e.g., greater than 100 meters, standoff from the detection apparatus, explosive, and potential harm and may be operated by a single member of an explosive ordnance disposal (EOD) team. The sUAS may be implemented as an easy-to-operate, small vertical take-off and landing (VTOL) aircraft with a set of optical, thermal, and chemical detection modules for detecting an IED by aerial surveillance, confirming the existence of explosives, and providing options for detonating the IED electrically or by delivery of a payload (e.g., object or device) to neutralize the IED while maintaining the sUAS itself safe from harm.

    Abstract translation: 一个小型无人驾驶空中系统（sUAS）用于远程检测隐藏的爆炸装置，例如埋藏或隐藏的简易爆炸装置（IED），并且在sUAS或其他人员的操作员或其他人员停留时，将设备爆炸或解除武装 安全距离。 sUAS系统可以在延长的，例如大于100米的范围内操作，与检测装置的对立，爆炸和潜在的危害，并且可以由单个爆炸物处理（EOD）团队的成员来操作。 该系统可以作为一个易于操作的小型垂直起降飞机（VTOL）实施，具有一套光学，热和化学检测模块，用于通过空中监视来检测IED，确认爆炸物的存在， 并提供引导IED的选项，或通过传送有效载荷（例如物体或设备）来中和IED，同时保持sUAS本身免受伤害。

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