TETHERING SYSTEM AND METHOD FOR REMOTE DEVICE
    192.
    发明申请
    TETHERING SYSTEM AND METHOD FOR REMOTE DEVICE 有权
    远程设备的计费系统和方法

    公开(公告)号:US20140259549A1

    公开(公告)日:2014-09-18

    申请号:US13804984

    申请日:2013-03-14

    Abstract: A tethering system for a remote-controlled device comprising a tether line having a first end adapted to be connected to a ground support and a second end adapted to be connected to the remote-controlled device. The system further includes an anchor-point disposed between the first and second ends of the tether line, the anchor point having an eyelet for securing the tether line and allowing the tether line to slide through the eyelet during use. The anchor-point and eyelet enable the tether line to flex or bend and the remote-controlled device to maneuver one or more of over or around the target area without interfering with any nearby obstructions.

    Abstract translation: 一种用于遥控装置的系绳系统,包括具有适于连接到地面支架的第一端的系绳线和适于连接到遥控装置的第二端。 系统还包括设置在系绳线的第一和第二端之间的锚定点,锚定点具有用于固定系绳的孔眼,并且允许系绳在使用期间通过孔眼滑动。 锚点和孔眼使得系绳弯曲或弯曲,并且远程控制装置在目标区域周围或周围操纵一个或多个,而不会干扰任何附近的障碍物。

    Unmanned vehicle and system
    193.
    发明授权
    Unmanned vehicle and system 有权
    无人车和系统

    公开(公告)号:US08788119B2

    公开(公告)日:2014-07-22

    申请号:US12964500

    申请日:2010-12-09

    Abstract: An unmanned vehicle is provided. The unmanned vehicle includes a navigation system configured to navigate the unmanned vehicle relative to a beam of energy emitted from a beam source, a power receiver configured to receive energy from the beam, and an energy storage system configured to store received energy for use in selectively powering the unmanned vehicle.

    Abstract translation: 提供无人驾驶车辆。 该无人驾驶车辆包括导航系统,该导航系统被配置为相对于从射束源发射的能量束导航无人驾驶车辆;被配置为从该波束接收能量的功率接收器以及被配置为存储用于选择性地使用的接收能量的能量存储系统 为无人驾驶车辆供电。

    High Altitude, Long Endurance, Unmanned Aircraft and Methods of Operation Thereof
    194.
    发明申请
    High Altitude, Long Endurance, Unmanned Aircraft and Methods of Operation Thereof 有权
    高海拔,长寿命,无人驾驶飞机及其操作方法

    公开(公告)号:US20140195150A1

    公开(公告)日:2014-07-10

    申请号:US13525045

    申请日:2012-06-15

    Abstract: Embodiments include one or more high altitude, long endurance (HALE) unmanned aircraft (110) capable of persistent station-keeping having one or more electromagnetic (IR/Visual/RF) sensor elements or suites (112, 337) for purposes of survey and/or signal gathering. Embodiments include one or more high altitude, long endurance (HALE) unmanned aircraft (110) capable of persistent station-keeping having a directable laser (331). Embodiments include a group of four or more high altitude, long endurance (HALE) unmanned aircraft (611-614) configured as GPS repeaters.

    Abstract translation: 实施例包括一个或多个能够持续驻留的具有一个或多个电磁(IR / Visual / RF)传感器元件或套件(112,337)的高空,长寿命(HALE)无人驾驶飞机(110),用于测量和 /或信号收集。 实施例包括能够持续驻留具有可定向激光(331)的一个或多个高空,长寿命(HALE)无人飞行器(110)。 实施例包括配置为GPS中继器的一组四个或更多的高空,长寿命(HALE)无人飞行器(611-614)。

    Helicopter with multi-rotors and wireless capability
    195.
    发明授权
    Helicopter with multi-rotors and wireless capability 有权
    具有多转子和无线能力的直升机

    公开(公告)号:US08774982B2

    公开(公告)日:2014-07-08

    申请号:US13200986

    申请日:2011-10-06

    Abstract: The present invention relates to a helicopter having a modular airframe, with multiple layers which can be connected easily, the layers which house the electronics (autopilot and navigation systems), batteries, and payload (including camera system) of the helicopter. The helicopter has four, six, and eight rotors, which can be easily changed via removing one module of the airframe. In one embodiment, the airframe has a vertical stacked appearance, and in another embodiment, a domed shape (where several of the layers are stacked internally). In one embodiment, there is a combination landing gear and camera mount. The helicopter allows for simple flight and usage by remote control, and non-remote control, users.

    Abstract translation: 本发明涉及一种具有模块化机身的直升机,其具有容易连接的多层,容纳直升机的电子设备(自动驾驶仪和导航系统),电池和有效载荷(包括照相机系统)的层。 直升机有四个,六个和八个转子,可以通过卸下机身的一个模块轻松更换。 在一个实施例中,机身具有垂直的堆叠外观,并且在另一个实施例中,圆顶形状(其中几个层内部堆叠)。 在一个实施例中,存在组合起落架和相机安装座。 直升机允许通过遥控器和非遥控器,用户进行简单的飞行和使用。

    REMOTE DETECTION, CONFIRMATION AND DETONATION OF BURIED IMPROVISED EXPLOSIVE DEVICES
    196.
    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

    Inventor: Farrokh Mohamadi

    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。

    Automatic Taking-Off And Landing System
    197.
    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

    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。

    ANTI-COLLISION LIGHTING SYSTEMS AND METHODS FOR A MICRO AERIAL VEHICLE
    199.
    发明申请
    ANTI-COLLISION LIGHTING SYSTEMS AND METHODS FOR A MICRO AERIAL VEHICLE 有权
    防撞照明系统和微型航空器的方法

    公开(公告)号:US20090303081A1

    公开(公告)日:2009-12-10

    申请号:US12133040

    申请日:2008-06-04

    CPC classification number: B64D47/06 B64C2201/141 B64C2201/145

    Abstract: Systems and methods for anti-collision lights on a UAV. A method for passive anti-collision lights on a Micro-Aerial Vehicle (“MAV”) including determining a location of the MAV using a flight management computer configured to fly the MAV on a programmed path using data from a global positioning system and an inertial navigation system. The flight management system transmits light activation data and selectively activates at least one navigation light located on a visible surface of the MAV using the light activation data from the flight management computer.

    Abstract translation: 无人机上防碰撞灯的系统和方法。 一种在微型飞行器(MAV)上的被动防碰撞灯的方法,包括使用飞行管理计算机确定MAV的位置,所述飞行管理计算机被配置为使用来自全球定位系统和惯性的数据的编程路径飞行MAV 导航系统。 飞行管理系统透射光激活数据,并使用来自飞行管理计算机的光激活数据选择性地激活位于MAV的可视表面上的至少一个导航灯。

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