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1.发明申请公开(公告)号：US20170370678A1
公开(公告)日：2017-12-28
申请号：US15641079
申请日：2017-07-03
CPC分类号： F41G7/306 , F41G7/2246 , F41G7/2266 , F41G7/2286 , F41G7/303 , G01S5/14 , G01S13/003 , G01S13/42 , G01S13/66 , G01S13/883 , G05D1/0088
摘要： A spatially-distributed architecture (SDA) of antennas transmits respective uniquely coded signals. A first receiver having a known position in a coordinate system defined by the SDA receives reflected versions of the uniquely coded signals. A first processor receives the reflected versions of the uniquely coded signals and identifies a position of a non-cooperative object in the coordinate system. A platform having a second receiver receives non-reflected versions of the uniquely coded signals. The platform determines a position of the platform in the coordinate system. In an example, the platform uses a self-determined position and a position of the non-cooperative object communicated from the SDA to navigate or guide the platform relative to the non-cooperative object. In another example, the platform uses a self-determined position and information from an alternative signal source in a second coordinate system to guide the platform. Guidance solutions may be generated in either coordinate system.
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公开(公告)号：US09633437B2
公开(公告)日：2017-04-25
申请号：US14173796
申请日：2014-02-05
申请人： Jahangir S Rastegar
发明人： Jahangir S Rastegar
CPC分类号： G06T7/285 , F41G7/30 , F41G7/306 , F42B15/01 , G05D1/12 , G06K9/00523 , G06K2017/0045 , G06K2209/21 , G06T7/20
摘要： A method for displaying successive image frames on a display. The method including: processing image data containing the successive image frames to identify features in an image frame and to display the image frame to a user with two or more of the identified features highlighted; manually selecting one of the identified features by a user; determining a portion of a subsequent image frame in which the selected feature is likely to be present; and if the selected feature is found in the portion of the subsequent image frame, displaying the subsequent image frame to change the position of the selected feature.
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公开(公告)号：US20160195365A1
公开(公告)日：2016-07-07
申请号：US14590627
申请日：2015-01-06
发明人： BRUCE WINKER , MILIND MAHAJAN , DON TABER , BRIAN GREGORY , JOHN MANSELL
摘要： A moving object command link system includes a transmitter which outputs a EM beam and a steering mechanism which directs the beam toward one or more objects, at least one of which is moving. The system may include a variable attenuator which modulates the average output power of the beam, and/or a divergence controller to maintain a desired beam size. The beam may be polarized, and the system may include a polarization modulator which changes the beam's polarization in accordance with a predetermined sequence and schedule. The system may include a 1×2 switch to selectively provide the beam to one of first and second outputs. A tiltable dichroic beam splitter may be used to couple beams received from first and second objects to track cameras having respective boresights that are offset with respect to each other.
摘要翻译： 移动物体指令链接系统包括输出EM光束的发射器和将光束引向一个或多个物体的转向机构，其中至少一个物体正在移动。 该系统可以包括调制波束的平均输出功率的可变衰减器和/或发散控制器以保持期望的波束尺寸。 光束可以是极化的，并且系统可以包括根据预定的顺序和时间表改变光束偏振的偏振调制器。 该系统可以包括1×2开关，用于选择性地将光束提供给第一和第二输出中的一个。 可以使用可倾斜的二向色光束分离器来将从第一和第二物体接收的光束耦合到具有相对于彼此偏移的各自的立体声的照相机。
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公开(公告)号：US20160048129A1
公开(公告)日：2016-02-18
申请号：US13839176
申请日：2013-03-15
申请人： Orbital ATK, Inc.
发明人： James Kolanek , Behshad Baseghi , David Sharpin , Anthony Visco , Falin Shieh
CPC分类号： G05D1/0022 , F41G7/306 , F41G7/308 , F41H11/02 , F42B15/01 , G01S13/883
摘要： Embodiments include engagement management systems and methods for managing engagement with aerial threats. Such systems include radar modules and detect aerial threats within a threat range of a base location. The systems also track intercept vehicles and control flight paths and detonation capabilities of the intercept vehicles. The systems are capable of communication between multiple engagement management systems and coordinated control of multiple intercept vehicles.
摘要翻译： 实施例包括参与管理系统和用于管理与空中威胁的接合的方法。 这样的系统包括雷达模块，并在基地区域的威胁范围内检测空中威胁。 这些系统还跟踪拦截车辆并控制拦截车辆的飞行路径和起爆能力。 这些系统能够在多个接合管理系统之间进行通信，并且能够对多个拦截车辆进行协调控制。
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公开(公告)号：US20130206896A1
公开(公告)日：2013-08-15
申请号：US13521661
申请日：2010-01-29
申请人： Fredrik Dicander
发明人： Fredrik Dicander
IPC分类号： F41G7/30
摘要： The object of the present invention is to provide an inventive guidance system for tracking and guiding at least one object, wherein said guidance system comprises a base station (1) including an optical imaging system (3) configured to determine the angular position vector of said at least one object (5, 15), an optical communication link for transmitting guidance control commands from said base station (1) to said at least one object (5, 15), and steering means provided on said at least one object (5, 15) for adjusting the direction of said at least one object (5, 15) in response to said guidance control commands. The invention also provides a corresponding guiding method.
摘要翻译： 本发明的目的是提供一种用于跟踪和引导至少一个物体的创新的引导系统，其中所述引导系统包括基站（1），基站（1）包括光学成像系统（3），其配置成确定所述 至少一个对象（5,15），用于从所述基站（1）向所述至少一个对象（5,15）发送引导控制命令的光通信链路，以及设置在所述至少一个对象（5）上的转向装置 ，15），用于响应于所述引导控制命令调节所述至少一个物体（5,15）的方向。 本发明还提供了相应的引导方法。
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6.发明申请METHODS AND APPARATUS FOR COMMUNICATIONS BETWEEN A FIRE CONTROL SYSTEM AND AN EFFECTOR 有权消防控制系统与效果器之间通讯的方法和装置公开(公告)号：US20110057070A1
公开(公告)日：2011-03-10
申请号：US12120432
申请日：2008-05-14
申请人： David A. Lance , Steven T. Siddens
发明人： David A. Lance , Steven T. Siddens
摘要： Methods and apparatus for communications between a fire control system and an effector according to various aspects of the present invention may include a communications link. The communications link may be coupled to a launcher for the effector and the effector. The communications link is detachably coupled to at least one of the launcher and the effector. The communications link may be adapted to transmit a fire control solution to the effector after initiating the launch.
摘要翻译： 根据本发明的各个方面的消防控制系统和效应器之间的通信的方法和装置可以包括通信链路。 通信链路可以耦合到用于效应器和效应器的发射器。 通信链路可拆卸地耦合到发射器和效应器中的至少一个。 通信链路可以适于在发起启动之后将消防控制解决方案传送到效应器。
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公开(公告)号：US20040196196A1
公开(公告)日：2004-10-07
申请号：US10475488
申请日：2004-05-21
发明人： Axel Stiller
IPC分类号： H01Q001/28
CPC分类号： H01Q13/085 , F41G7/306
摘要： The invention relates to antenna elements for the UHF and VHF range for antennas of an airborne vehicle with empennage parts. These antenna elements are integrated into the empennage parts (L) which are made of a dielectric material and are configured in such a way that they radiate directionally broadband in flight direction. The empennage parts are made, for example, of ceramic, and the antenna elements are embedded therein or are applied to their surface. The antenna elements (A) are preferably expanding Vivaldi-type slot radiators that are halved along their axis of symmetry and use the airborne vehicle (F) as an electrical mirror. Arranging the antenna elements in the area of the rudder maximizes both the aperture and the distance between the phase centers of the individual elements, but no additional volume is required for the antennas.
摘要翻译： 本发明涉及用于具有尾翼部件的机载车辆的天线的UHF和VHF范围的天线元件。 这些天线元件集成到由电介质材料制成的尾翼部件（L）中，并且被配置成使得它们在飞行方向上辐射定向宽带。 尾翼部件例如由陶瓷制成，并且天线元件嵌入其中或施加到其表面。 天线元件（A）优选是扩展的Vivaldi型槽式散热器，其沿其对称轴线减半，并使用机载车辆（F）作为电反射镜。 在方向舵区域内布置天线元件使孔径和各个元件的相位中心之间的距离最大化，但是天线不需要额外的体积。
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8.发明授权Data insertion system for modulating the carrier of a radio voice transmitter with missile control signals 失效用于利用导弹控制信号调制无线电话音发射机载波的数据插入系统
公开(公告)号：US5691531A
公开(公告)日：1997-11-25
申请号：US744284
申请日：1996-11-06
申请人： Gordon L. Harris , Neil A. Levy , Daniel R. Weisz
发明人： Gordon L. Harris , Neil A. Levy , Daniel R. Weisz
摘要： A microcomputer with a modem is programmed with information for controlling a flight control computer on a missile. The microcomputer is carried on an aircraft from which the missile is controlled. The pilot of the aircraft has a keypad for setting the target coordinates in the microcomputer. The audio signals from the microcomputer modem are fed to the voice communications system of the aircraft so as to modulate the carrier of the transmitted signal. This signal is received by the receiver on the missile and demodulated and employed to control signals for the missile in the missile flight control computer. The pilot of the aircraft sets in target coordinates for the missile on a keypad connected to the microcomputer.
摘要翻译： 具有调制解调器的微型计算机具有用于控制导弹上的飞行控制计算机的信息。 微型计算机载有导弹受控的飞机上。 飞机的飞行员具有用于设置微型计算机中的目标坐标的小键盘。 来自微机调制解调器的音频信号被馈送到飞行器的语音通信系统，以便调制发射信号的载波。 该信号由导弹上的接收器接收并解调并用于控制导弹飞行控制计算机中导弹的信号。 飞机的飞行员在与微型计算机连接的键盘上设置导弹的目标坐标。
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公开(公告)号：US5544843A
公开(公告)日：1996-08-13
申请号：US749652
申请日：1991-08-01
申请人： William M. Johnson
发明人： William M. Johnson
IPC分类号： F41G7/30
摘要： A space-based command guidance controller and controlled deliverable traveling at speeds of about Mach five are cooperative to cause the deliverable to follow a coherent designator beam controlled by the space-based command guidance controller to be delivered to a target location, eventually designated by the beam along an over-the-horizon trajectory, and into a target thereat with surgical-like precision. The command guidance controller includes an optical tracker and coherent designator laser assembly and an inertially-stabilized tracker that are cooperative to produce a command guidance signal representative of that controlled deliverable maneuver that enables the controlled deliverable, upon the execution thereof, to conform its trajectory to the intended trajectory, and eventually, to impact the intended target. The controlled deliverable includes an autopilot that executes the maneuver represented by the command guidance signal in order to bring the controlled deliverable into local conformance to the intended trajectory. The controlled deliverable includes an optical roll sensor having a negligible scale-factor-error. The intended target location may include a static and/or a dynamic target object.
摘要翻译： 基于空间的指挥指导控制器和以约5马赫的速度行进的受控交付物是协调的，以使得可交付物遵循由基于空基的指挥指导控制器控制的相干指示符波束被传递到目标位置，最终由 沿着地平线上的轨迹射入，并以外科手术的精度进入目标。 命令指导控制器包括光学跟踪器和相干指示器激光器组件和惯性稳定的跟踪器，它们协作以产生代表该受控可交付操作的命令指导信号，使其能够在其执行时使其受控交付符合其轨迹 预期轨迹，最终影响预期目标。 受控交付物包括执行由指令指导信号表示的操纵的自动驾驶仪，以便将受控交付物局部地符合预期的轨迹。 受控交付物包括具有可忽略的比例因子误差的光学辊传感器。 预期的目标位置可以包括静态和/或动态目标对象。
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10.发明授权
公开(公告)号：US5541839A
公开(公告)日：1996-07-30
申请号：US328060
申请日：1994-10-24
申请人： Uwe Mitzkus , Reiner Eckhardt
发明人： Uwe Mitzkus , Reiner Eckhardt
IPC分类号： F41G7/00 , F41G7/30 , G06F165/00 , F41F7/00 , G06F171/00
摘要： The interface arrangement is provided for data transfer between a carrier aircraft and a missile which is to be launched from the carrier aircraft and which includes a target seeking head. The missile is connected to the carrier aircraft through a connecting cable which contains a small number of wires sufficient for transferring analog data and which is detachable upon launch. For selectively operating the carrier aircraft in conjunction with a missile which is equipped with either (i) a target seeking head producing analog target deviation data or (ii) a image processing target seeking head, at least two interfaces are connected to the connecting cable. One of the interfaces is designed for data transfer via the connecting cable to and from the target seeking head producing analog target deviation data. An other one of the interfaces is designed for data transfer via the connecting cable to and from a image processing target seeking head. A controller enables selective connection of the connecting cable to either one of the two interfaces. The controller responds to identifying signals signalling the type of target seeking head and automatically activating a respective one of the interfaces.
摘要翻译： 该接口装置被提供用于承运飞机与将从承运飞机发射并包括目标寻求头的导弹之间的数据传输。 导弹通过连接电缆连接到载体飞机，连接电缆包含足够数量的电线，用于传输模拟数据，并且在发射时可拆卸。 为了与携带有（i）目标寻求头产生模拟目标偏差数据的导弹或（ii）图像处理目标寻求头部）的导弹有选择地操作载体飞行器，至少两个接口连接到连接电缆。 其中一个接口设计用于通过连接电缆到达目标寻求头和从目标寻求头产生模拟目标偏差数据的数据传输。 另一个接口被设计用于经由连接电缆到和从图像处理目标寻找头的数据传输。 控制器可以将连接电缆选择性连接到两个接口之一。 控制器响应于识别信号，寻找目标寻找头的类型并自动激活相应的一个接口。
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