Multifunctional de-icing/anti-icing system
    51.
    发明授权
    Multifunctional de-icing/anti-icing system 有权
    多功能除冰/防冰系统

    公开(公告)号:US08931740B2

    公开(公告)日:2015-01-13

    申请号:US13522368

    申请日:2010-01-14

    CPC classification number: H05B3/145 B64C3/20 B64C3/26 B64D15/12 H05B2214/04

    Abstract: A de-icing/anti-icing system including at least two conductive structures embedded in an article that includes an outer surface designed as an aerodynamic surface. At least one of the conductive structures is arranged adjacent the outer surface. A control unit adapted to control the energy supply to the conductive structures for generating heat to the outer surface. A first of the conductive structures includes a first conductive nano structure and a second of the conductive structures includes a second conductive nano structure. A conductive property of the first of the conductive structures differs from a conductive property of the second of the conductive structures. The first conductive nano structure serves as a heating conductor and the second conductive nano structure serves as a heating element. The first and second conductive nano structures are embedded in a common plane of a resin layer forming the outer surface.

    Abstract translation: 一种除冰/防冰系统,其包括嵌入制品中的至少两个导电结构,其包括被设计为空气动力学表面的外表面。 导电结构中的至少一个布置成与外表面相邻。 控制单元,其适于控制向导电结构的能量供应,以向外表面产生热量。 第一导电结构包括第一导电纳米结构,第二导电结构包括第二导电纳米结构。 第一导电结构的导电性与第二导电结构的导电性不同。 第一导电纳米结构用作加热导体,第二导​​电纳米结构用作加热元件。 第一和第二导电纳米结构嵌入到形成外表面的树脂层的共同平面中。

    Evaluating system and method for shooting training
    54.
    发明授权
    Evaluating system and method for shooting training 有权
    评估射击训练的系统和方法

    公开(公告)号:US08876533B2

    公开(公告)日:2014-11-04

    申请号:US12494975

    申请日:2009-06-30

    Applicant: Alf Axerud

    Inventor: Alf Axerud

    CPC classification number: F41J11/00 F41G3/26 F41J5/00

    Abstract: An evaluation system for shooting training. The evaluation system is arranged to determine from which shooter fired ammunition detected by a target system originates. The evaluation system includes a receiver unit arranged to receive shooter messages from a plurality of weapon systems and to receive a target message from the target system. Each shooter message includes time marked firing information and first pairing information related to a weapon of the weapon system. Each target message includes time marked hit/miss information and second pairing information related to a target of the target system. The evaluation system further includes a processing unit arranged to pair the target with one associated weapon based on the target message and each respective shooter message. Also, a method for determining from where ammunition detected at a target was fired.

    Abstract translation: 射击训练评估系统。 评估系统被安排来确定目标系统检测到的射击枪发射的射弹。 评估系统包括接收器单元,其被布置成从多个武器系统接收射击者消息并从目标系统接收目标消息。 每个射击者消息包括与武器系统的武器相关的时间标记的射击信息和第一对配对信息。 每个目标消息包括与目标系统的目标相关的时间标记的命中/未命中信息和第二配对信息。 评估系统还包括处理单元,其被配置为基于目标消息和每个相应的射手消息将目标与一个相关武器进行配对。 另外,确定从目标处检测到弹药的方法被解雇。

    CALCULATING TIME TO GO AND SIZE OF AN OBJECT BASED ON SCALE CORRELATION BETWEEN IMAGES FROM AN ELECTRO OPTICAL SENSOR
    56.
    发明申请
    CALCULATING TIME TO GO AND SIZE OF AN OBJECT BASED ON SCALE CORRELATION BETWEEN IMAGES FROM AN ELECTRO OPTICAL SENSOR 有权
    基于来自电光传感器的图像之间的尺度相关的计算对象的大小和尺寸

    公开(公告)号:US20140278048A1

    公开(公告)日:2014-09-18

    申请号:US14289201

    申请日:2014-05-28

    Applicant: SAAB AB

    Inventor: Jimmy Jonsson

    CPC classification number: G08G5/045 G06K9/00805 G08G5/0021

    Abstract: A method for calculating a Time To Go value between a vehicle and an intruding object. First and second images of the object are retrieved at first and second points of time. A scaling factor is selected and the second image scaled with the scale factor. The scaled image is resampled to a set position. Correlation values are calculated between the first image and the resampled scaled image for different horizontal displacements and/or different vertical displacements for the resampled scaled image. A maximum correlation value is found based on the correlation values. Selecting the scaling factor, resampling, calculating the correlation values, and finding the maximum correlation values are repeated a second predetermined number of times. A largest maximum correlation value is found among the maximum correlation values and the scale factor associated with the largest maximum correlation value. The Time To Go is calculated based on the associated scale factor.

    Abstract translation: 一种用于计算车辆和入侵物体之间的“到达时间”值的方法。 在第一和第二时间点检索对象的第一和第二图像。 选择缩放因子,第二个图像用比例因子缩放。 缩放图像被重新采样到设置位置。 对于不同的水平位移和/或重采样的缩放图像的不同垂直位移,在第一图像和重采样的缩放图像之间计算相关值。 基于相关值找到最大相关值。 选择缩放因子,重采样,计算相关值和找到最大相关值重复第二预定次数。 在最大相关值和与最大最大相关值相关联的比例因子之间找到最大最大相关值。 Time to Go是根据相关的比例因子计算的。

    METHOD AND SYSTEM FOR STEERING AN UNMANNED AERIAL VEHICLE
    57.
    发明申请
    METHOD AND SYSTEM FOR STEERING AN UNMANNED AERIAL VEHICLE 有权
    用于转向无人驾驶航空器的方法和系统

    公开(公告)号:US20140200744A1

    公开(公告)日:2014-07-17

    申请号:US14119006

    申请日:2011-05-26

    CPC classification number: B64C19/00 B64C39/024 G05D1/0094 G05D1/101

    Abstract: The present invention relates to a method for steering a UAV, Unmanned Aerial Vehicle, to enable a high level command of the UAV. The method comprising the steps of: determining (500) a reference position (200, 300, 400) related to a position (210, 310, 410) for a moving object (220, 320, 420) which the UAV should follow; calculating (515) a smoothed position (230, 330, 430) based on the reference position (200, 300, 400), wherein the smoothed position (230, 330, 430) is calculated so that the smoothed position (230, 330, 430) moves more smoothly than the reference position (200, 300, 400); and steering (525) the UAV so that UAV follows the smoothed position (230, 330, 430).

    Abstract translation: 本发明涉及一种无人机无人驾驶飞行器的转向方法,以实现无人机的高级命令。 该方法包括以下步骤:确定(500)与UAV应该遵循的移动物体(220,320,420)相关的位置(210,310,410)的参考位置(200,300,400); 基于所述参考位置(200,300,400)计算(515)平滑位置(230,330,430),其中计算所述平滑位置(230,330,430),使得平滑位置(230,330,430) 430)比基准位置(200,300,400)更平滑地移动; 和转向(525)UAV,使得UAV遵循平滑位置(230,330,430)。

    Safe termination of UAV
    58.
    发明授权
    Safe termination of UAV 有权
    无人机的安全终止

    公开(公告)号:US08755950B2

    公开(公告)日:2014-06-17

    申请号:US13058105

    申请日:2009-08-06

    Inventor: Rikard Johansson

    CPC classification number: G05D1/0022

    Abstract: A termination system that transmits on a cyclic basis, from a control station to an unmanned vehicle, pairs of mutually dependent code and counter values whose dependency is determined by a termination algorithm. The vehicle has knowledge of the algorithm and can hence validate a received code/counter pair using the same algorithm. If the received code/counter pair is invalid, the vehicle can decide to self-terminate. The control station includes a termination actuator that allows the vehicle to be remotely terminated by invalidating, when actuated by an operator, the code/counter pairs that are transmitted to the vehicle.

    Abstract translation: 从循环的基础上从控制站向无人驾驶车辆发送相互依赖的代码对和计数器值的终止系统,其依赖性由终止算法确定。 车辆具有该算法的知识,并且因此可以使用相同的算法来验证接收到的代码/计数器对。 如果接收到的代码/计数器对无效,则车辆可以自行终止。 控制站包括终端致动器,其允许当由操作员致动时将车辆的代码/计数器对发送到车辆而使车辆远程终止。

    Dual frequency antenna aperture
    59.
    发明授权
    Dual frequency antenna aperture 有权
    双频天线孔径

    公开(公告)号:US08723748B2

    公开(公告)日:2014-05-13

    申请号:US13141427

    申请日:2008-12-22

    Applicant: Bengt Svensson

    Inventor: Bengt Svensson

    CPC classification number: H01Q21/28 H01Q9/16 H01Q9/28 H01Q13/08 H01Q13/10

    Abstract: An antenna structure including at least two stacked antenna apertures, a first antenna aperture with first antenna elements and at least a second antenna aperture with second antenna elements. The antenna structure is arranged for operation in at least a high and a low frequency band. The first antenna elements are arranged for operation in the high frequency band and the second antenna elements for operation in the low frequency band. The first antenna elements are arranged to have a polarization substantially perpendicular to the polarization of the second antenna elements. The second antenna elements are arranged in at least one group and each of the group includes a number of second antenna elements coupled in series and arranged to have a common feeding point on a straight feeding structure. One feeding structure is located adjacent to each group of second antenna elements. The direction of the feeding structure is substantially perpendicular to the polarization of the first antenna elements. A corresponding method and a radar system including the antenna structure.

    Abstract translation: 包括至少两个堆叠的天线孔的天线结构,具有第一天线元件的第一天线孔和具有第二天线元件的至少第二天线孔。 天线结构布置成在至少高频和低频带中操作。 第一天线元件布置成在高频带中操作,第二天线元件用于在低频带中操作。 第一天线元件被布置成具有基本上垂直于第二天线元件的极化的偏振。 第二天线元件被布置在至少一个组中,并且每个组包括多个串联耦合的第二天线元件,并且布置成在直线馈送结构上具有共同的馈电点。 一个馈送结构位于每组第二天线元件附近。 馈送结构的方向基本上垂直于第一天线元件的极化。 包括天线结构的相应方法和雷达系统。

    Device at an airborne vehicle and a method for collision avoidance
    60.
    发明授权
    Device at an airborne vehicle and a method for collision avoidance 有权
    飞机上的装置和避免碰撞的方法

    公开(公告)号:US08700231B2

    公开(公告)日:2014-04-15

    申请号:US12003307

    申请日:2007-12-21

    Applicant: Erik Skarman

    Inventor: Erik Skarman

    CPC classification number: G08G5/0078 G08G5/045

    Abstract: A device at an airborne vehicle including a flight control system configured to control the behavior of the airborne vehicle based on acceleration commands, a first control unit configured to provide the acceleration commands to the flight control system, and a collision avoidance unit. The collision avoidance unit includes a detection unit arranged to detect whether the airborne vehicle is on a collision course and a second control unit arranged to feed forced acceleration commands to the flight control system upon detection that the airborne vehicle is on a collision course. A method for collision avoidance in an airborne vehicle.

    Abstract translation: 一种机载装置,包括:飞行控制系统,被配置为基于加速指令来控制机载车辆的行为;第一控制单元,被配置为向飞行控制系统提供加速指令;以及防撞单元。 碰撞避免单元包括检测单元,该检测单元被布置为检测空中交通工具是否处于碰撞过程;以及第二控制单元,其布置成在检测到空中交通工具处于碰撞过程时将强制加速命令提供给飞行控制系统。 一种机载碰撞避免的方法。

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