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公开(公告)号：US20140138473A1
公开(公告)日：2014-05-22
申请号：US13552038
申请日：2012-07-18
申请人： Wai YU
发明人： Wai YU
IPC分类号： F41G7/22
CPC分类号： F41G7/263
摘要： Missile guidance involving projection of laser light to define a Laser Information Field (LIF) is augmented by interposition of information pulses, interleaved between laser emissions establishing the LIF. Information pulses encode further information for receipt by a missile, such as an angle of roll of a missile launch platform from which the LIF is emitted.
摘要翻译： 涉及投射激光以定义激光信息场（LIF）的导弹引导通过插入建立LIF的激光发射之间交错的信息脉冲来增强。 信息脉冲编码进一步的信息以供导弹接收，例如发射LIF的导弹发射平台的滚动角度。
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公开(公告)号：US20060098710A1
公开(公告)日：2006-05-11
申请号：US11317743
申请日：2005-12-23
申请人： Ulrich Kienitz
发明人： Ulrich Kienitz
IPC分类号： G01K1/14
CPC分类号： F41G7/263 , G01J5/08 , G01J5/0803 , G01J5/0831 , G01J5/0859 , G01J5/089 , G01J5/0896
摘要： A sighting device is provided which is used to produce an optically perceptible target marking on an object. The sighting device includes one or more light sources for providing at least two sighting rays. A precision target marking is produced in such a manner that each of the sighting rays is directed onto a respective optical component enabling both of the sighting rays to be split on a respective illumination plane in such a manner that at least two illumination planes intersect at an angle. The point of intersection forms the target marking. A measuring, working and/or operating device is optionally provided which can be used with or without contact and which interacts with an object of any type at a predetermined target location. The target location can be detected by means of the inventive sighting device.
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公开(公告)号：US5601255A
公开(公告)日：1997-02-11
申请号：US438018
申请日：1995-05-08
申请人： Rudolf Romer , Gerd Wollmann , Helmut Misoph
发明人： Rudolf Romer , Gerd Wollmann , Helmut Misoph
IPC分类号： F41G7/26
摘要： A method and an apparatus for flight path correction of one or more projectiles (2-6) with the aid of a guide beam (9), wherein target data, such as speed, range and direction of movement, are continuously acquired in a fire-guidance system associated with the firing device (1), for example, an automatic cannon, and are transmitted to the laser apparatus (21) that produces the guide beam (9), and wherein each projectile includes a receiving apparatus (31) which receives the guide beam (9). To be able to correct, in a simple manner with a pulse correction, both individual projectiles as well as a plurality of projectiles flying closely behind one another in time and having different courses, the guide beam (9) is aimed toward the collision point (15) calculated on the basis of the target data, and the guide beam (9) is subdivided into a plurality, at least five, partial beams (guide beam segments 10-14) including a central guide beam segment (10) which is aimed at the collision point (15) and around which the remaining partial beams or beam segments are disposed. The guide beam segments (10-14) are all modulated differently. Each projectile (2-6), with the aid of its respective receiving apparatus (31), then determines the angular position necessary for the correction, with respect to the collision point (15), from the modulation of the respective received guide beam segment (10-14).
摘要翻译： 借助于导向梁（9）的一个或多个射弹（2-6）的飞行路径校正的方法和装置，其中诸如速度，范围和运动方向的目标数据在火中连续获取 与点火装置（1）相关联的指示系统，例如自动炮，并被传送到产生导向梁（9）的激光装置（21），并且其中每个抛射体包括接收装置（31），其中 接收引导梁（9）。 为了能够以简单的方式校正脉冲，两个单独的射弹以及多个在时间上彼此紧密地相互悬挂并且具有不同的路线的抛射体，引导梁（9）被瞄准到碰撞点 基于目标数据计算的引导光束（9）被细分成多个至少五个部分光束（引导光束段10-14），其包括目标的中心引导光束段（10） 在碰撞点（15）处，并且在其周围设置剩余的部分光束或光束段。 引导光束段（10-14）都被不同地调制。 然后借助各自的接收装置（31），每个抛射体（2-6）根据相应的接收引导光束段的调制确定相对于碰撞点（15）进行校正所需的角位置 （10-14）。
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公开(公告)号：US5219132A
公开(公告)日：1993-06-15
申请号：US356700
申请日：1982-03-03
IPC分类号： F41G7/26
CPC分类号： F41G7/263
摘要： A gyroscopically stabilized optical seeker for use in a cannon-launched projectile is shown to include a gimbal arrangement wherein a two-axis rate gyroscope and associated torque motors are utilized to attain the requisite stabilization however such seeker is oriented with respect to such projectile, the two-axis rate gyroscope being arranged so that the complete optical system, including the detector unit, may be mounted on the inner gimbal.
摘要翻译： 用于炮弹发射的抛射体的陀螺稳定的光学探测器显示为包括万向节布置，其中使用双轴速率陀螺仪和相关联的扭矩马达来获得必要的稳定性，但是这种探测器相对于这种射弹取向， 布置两轴速率陀螺仪，使得包括检测器单元的完整光学系统可以安装在内部万向节上。
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公开(公告)号：US4100404A
公开(公告)日：1978-07-11
申请号：US704894
申请日：1976-07-13
摘要： A beam projector is provided by a plurality of coded reticles mounted on a spinning disc and illuminated by a laser source. In order to maintain a constant irradiance on a receiver variably located in space a pseudo-zoom assembly is provided including a moveable source and/or condenser optics. Also, plural focal length optics are employed to expand the range over which the constant irradiance is maintained beyond that realizable by the pseudo-zoom assembly itself.
摘要翻译： 光束投影仪由安装在旋转盘上并由激光源照射的多个编码标线提供。 为了在可变地位于空间中的接收器上保持恒定的辐照度，提供包括可移动源和/或冷凝器光学器件的伪变焦组件。 此外，采用多个焦距光学器件来扩大恒定辐照度的范围，超出可由伪变焦组件本身实现的范围。
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公开(公告)号：US08502127B2
公开(公告)日：2013-08-06
申请号：US13547461
申请日：2012-07-12
申请人： Allister McNeish
发明人： Allister McNeish
IPC分类号： F42B15/01
摘要： An optical guidance system for guiding a projectile is disclosed. The optical guidance system includes a laser, a first and second cylindrical holographic lenses and a variable zoom lens. The laser generates a laser beam, and the first and second cylindrical holographic lenses transform the laser beam into a x-direction and y-direction scan patterns, respectively. The variable zoom lens projects the x-direction and y-direction scan patterns in the form of multiple scan fields, each within a scan corridor, in order to guide a projectile along a flight path towards a target.
摘要翻译： 公开了一种用于引导射弹的光学引导系统。 光学引导系统包括激光器，第一和第二圆柱形全息透镜和可变焦距透镜。 激光产生激光束，并且第一和第二圆柱全息透镜分别将激光束变换成x方向和y方向扫描图案。 可变变焦镜头以扫描走廊中的多个扫描场的形式投影x方向和y方向扫描图案，以便沿着飞行路径朝向目标引导射弹。
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7.发明授权Sighting device and additional device for measuring, working, and/or operating with or without contact 有权瞄准装置和附加装置，用于测量，工作和/或操作有或没有接触公开(公告)号：US07545492B2
公开(公告)日：2009-06-09
申请号：US11317743
申请日：2005-12-23
申请人： Ulrich Kienitz
发明人： Ulrich Kienitz
IPC分类号： G01C9/00
CPC分类号： F41G7/263 , G01J5/08 , G01J5/0803 , G01J5/0831 , G01J5/0859 , G01J5/089 , G01J5/0896
摘要： A sighting device is provided which is used to produce an optically perceptible target marking on an object. The sighting device includes one or more light sources for providing at least two sighting rays. A precision target marking is produced in such a manner that each of the sighting rays is directed onto a respective optical component enabling both of the sighting rays to be split on a respective illumination plane in such a manner that at least two illumination planes intersect at an angle. The point of intersection forms the target marking. A measuring, working and/or operating device is optionally provided which can be used with or without contact and which interacts with an object of any type at a predetermined target location. The target location can be detected by means of the inventive sighting device.
摘要翻译： 提供了一种用于在物体上产生光学上可感知的目标标记的瞄准装置。 瞄准装置包括用于提供至少两个瞄准射线的一个或多个光源。 以这样的方式产生精密目标标记，使得每个瞄准光线被引导到相应的光学部件上，使得能够使两个瞄准光线在相应的照明平面上分开，使得至少两个照明平面在 角度。 交点形成目标标记。 任选地提供测量，工作和/或操作装置，其可以在有或没有接触的情况下使用，并且与预定目标位置处的任何类型的物体相互作用。 可以通过本发明的瞄准装置来检测目标位置。
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公开(公告)号：US5410398A
公开(公告)日：1995-04-25
申请号：US67774
申请日：1979-08-20
申请人： Quentin D. Appert , Thomas E. Godfrey , David L. Hammond , Gary O. McFerson , Richard F. Odum , Raymond H. Ottoson
发明人： Quentin D. Appert , Thomas E. Godfrey , David L. Hammond , Gary O. McFerson , Richard F. Odum , Raymond H. Ottoson
摘要： A device for automatically compensating for dynamic boresight errors between a visual line of sight and the apparent center of a beam of radiation emitted by the device. The radiation emitted by the device is used to guide a "beam-riding" missile to its target. Different sectors of the beam radiated by the device are modulated by different codes so that the missile can sense the apparent center of the beam. Optics within the device sense the extent to which the visual line of sight deviates from the apparent center of the radiated beam by means of measurements upon the coincidence of the visual line of sight and the apparent center of the beam of radiation within the device. The device then alters the coding of the radiated beam so that the apparent center of the radiated beam maintains alignment with the visual line of sight.
摘要翻译： 用于自动补偿视觉视线与设备发射的辐射束的视在中心之间的动态视轴误差的装置。 该装置发射的辐射用于将“横梁”导弹引导到其目标。 由装置辐射的光束的不同扇区由不同的代码调制，使得导弹可以感测光束的表观中心。 装置内的光学器件通过视觉视线和装置内的辐射束的表观中心的一致性进行测量，感测到视线从辐射束的表观中心偏离的程度。 然后，该装置改变辐射束的编码，使得辐射束的表观中心保持与视线的对准。
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公开(公告)号：US5197691A
公开(公告)日：1993-03-30
申请号：US532885
申请日：1983-09-16
申请人： Max Amon , Nicholas B. Saccketti
发明人： Max Amon , Nicholas B. Saccketti
摘要： An optical arrangement for use in boresighting a plurality of optical paths utilized in a missile beam guidance system, to the target trackers used therewith. A boresight module optical bed supports a plurality of retro-reflective optical assemblies in a closely spaced array, and nearby is a rotational optical assembly in which is mounted an integrated laser system for providing beam guidance to a missile. The rotational optical assembly also contains a plurality of target trackers, and in a first operational mode, the laser of the rotational assembly is successively utilized in conjunction with the retro-reflective optical assemblies in order to accurately and conveniently boresight the trackers. Thereafter, the trackers are used in the acquisition and tracking of a target, and the laser is utilized for guiding the missile to intercept the target.
摘要翻译： 一种光学装置，用于将导弹束引导系统中使用的多个光学路径瞄准到与其一起使用的目标跟踪器。 视轴模块光学床以紧密间隔的阵列支撑多个后向反射光学组件，并且附近是旋转光学组件，其中安装有用于向导弹提供射束引导的集成激光系统。 旋转光学组件还包含多个目标跟踪器，并且在第一操作模式中，旋转组件的激光器与后向反射光学组件连续地被使用，以便精确地且方便地瞄准跟踪器。 此后，跟踪器被用于目标的获取和跟踪，并且激光被用于引导导弹拦截目标。
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公开(公告)号：USH299H
公开(公告)日：1987-07-07
申请号：US943360
申请日：1986-12-15
CPC分类号： F41G7/263
摘要： A method and apparatus for projecting a laser beam for communication or guidance purposes wherein transmitted energy goes directly to a receiver area without requiring services of slewing or tracking devices. The energy is precisely directed from a laser transmitter on a missile toward a receiver at a tracking area. By directing the laser energy from a source on the missile during flight and by performing phase conjugating amplification of this laser energy at a tracking area station, atmospheric distortions are removed from the return energy and beam broadening is limited only to the negligible effects of diffraction broadening of the return energy, with the laser return beam being directed almost exclusively back to the missile.
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