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21. 发明申请

WO2002070981A1 SYSTEME DE VISEE A POINTAGE LASER A TELEMETRE DESIGNATEUR 审中-公开
标题翻译：具有指示器范围的激光瞄准系统
公开(公告)号：WO2002070981A1
公开(公告)日：2002-09-12
申请号：PCT/FR2002/000806
申请日：2002-03-06
申请人： SAGEM S.A. , DUFRESNE DE VIREL, François
发明人： DUFRESNE DE VIREL, François
IPC分类号： F41G7/22
CPC分类号： F41G7/226 , F41G7/2293 , G01S3/786 , G01S3/7864 , G01S17/023
摘要： Le système de visée à pointage laser, du type comportant un télémètre désignateur (19) comprend des moyens (E) pour l'émission d'un faisceau de désignation et des moyens de réception (R) pour détecter et traiter la réflexion d'une tache lumineuse formée par ledit faisceau sur une cible, lesdits moyens de réception (R) sont aptes, en l'absence d'émission de faisceau de désignation par le télémètre, à détecter la réflexion d'une tache lumineuse formée sur une cible par un dispositif de désignation tiers, le système comportant des moyens aptes, lorsque les moyens de réception du télémètre détectent une telle tache lumineuse, à s'orienter automatiquement par rapport à la direction définie par ladite tache.
摘要翻译：本发明涉及一种激光瞄准瞄准系统，包括指示器测距仪（19），其包括用于发射指示激光束的装置（E）和用于检测和处理由所述光束形成的热点在目标上的反射的接收装置（R）所述接收装置（R）能够通过测距仪不指定光束发射，检测由第三指定装置形成在目标上的热点的反射，所述系统包括能够在接收装置检测时这种热点相对于由所述点限定的方向自动定向。

22. 发明申请

WO01077627A3 A SYSTEM FOR ROBOTIC CONTROL OF IMAGING DATA HAVING A STEERABLE GIMBAL MOUNTED SPECTRAL SENSOR AND METHODS 审中-公开
标题翻译：用于具有可转动的金属安装光谱传感器的成像数据的机器人控制系统及方法
公开(公告)号：WO01077627A3
公开(公告)日：2002-05-30
申请号：PCT/US2001/010255
申请日：2001-03-30
IPC分类号： F41G7/22 , G01J3/28
CPC分类号： F41G7/008 , F41G3/14 , F41G3/165 , F41G3/22 , F41G7/2213 , F41G7/2246 , F41G7/2253 , F41G7/2293 , G01J3/0202 , G01J3/0205 , G01J3/0235 , G01J3/0264 , G01J3/027 , G01J3/0278 , G01J3/0289 , G01J3/0291 , G01J3/06 , G01J3/10 , G01J3/2823 , G01J3/36 , G01J3/50
摘要： A robotically controlled steerable gimbal (30) mounted virtual broadband hyperspectral sensor (40) system and methods provide a highly mobile, rapidly responsive and innovative system of locating targets and exploiting hyperspectral and ultraspectral imaging and non-imaging signature information in real-time from an aircraft or ground vehicles (V) from overhead or standoff perspective in order to discriminate and identify unique spectral characteristics of the target. The system preferably has one or more mechanically integrated hyperspectral sensors (40) installed on a gimbal backbone and coboresighted with a similarly optional mounted color video camera and optional LASER (47) within an aerodynamically stable pod shell constructed for three-dimensional stabilization and pointing of the sensor on a direct overhead or off-nadir basis.
摘要翻译：一种机器人控制的可操纵万向节（30）安装的虚拟宽带高光谱传感器（40）系统和方法提供了一种高度移动，快速响应和创新的定位目标系统，并且可以实时地从高光谱和超光谱成像以及非成像签名信息中实时获取飞机或地面车辆（V），以便区分和识别目标的独特光谱特征。该系统优选地具有一个或多个机械集成的高光谱传感器（40），其安装在万向架骨架上并且与类似地可选的安装的彩色摄像机和可选的激光器（47）共同安装在空气动力学稳定的荚壳内，其被构造用于三维稳定和指向传感器基于直接开销或最低点。

23. 发明申请

WO00079324A1 SENSOR SYSTEM WITH RIGID-BODY ERROR CORRECTING ELEMENT 审中-公开
标题翻译：具有刚体错误校正元件的传感器系统
公开(公告)号：WO00079324A1
公开(公告)日：2000-12-28
申请号：PCT/US2000/016485
申请日：2000-06-14
IPC分类号： F41G7/22 , G02B26/10 , G02B27/00
CPC分类号： F41G7/2253 , F41G7/2213 , F41G7/2293 , G02B26/101
摘要： A sensor system includes a sensor, and an optical train adjustable to provide an optical beam to the sensor from a selected line of sight that may be varied. The optical train includes a wavefront error-introducing element in the optical train, which introduces a wavefront error that is a function of the selected line of sight. There is further a rigid-body wavefront error-correcting element in the optical train. The rigid-body wavefront error-correcting element has a spatially dependent correction structure with the nature of the correction being a function of the selected line of sight. The adjustment of the optical train to the selected line of sight moves the optical beam to the appropriate location of the rigid-body wavefront error-correcting element to correct for the corresponding introduced wavefront error of the wavefront error-introducing element at that selected line of sight.
摘要翻译：传感器系统包括传感器和可调整的光学列车，以从可能变化的所选视线提供光束到传感器。光学列车包括光学列车中的波前误差引入元件，其引入作为所选择的视线的函数的波前误差。在光学列车中还有一个刚体波前纠错元件。刚体波前纠错元件具有空间依赖的校正结构，校正的性质是所选择的视线的函数。将光学系统调整到所选择的视线将光束移动到刚体波前纠错元件的适当位置，以校正波导误差引入元件在该选定行的对应的引入波前误差视线。

24. 发明申请

WO00047943A1 TARGET DETECTION METHOD AND DEVICE 审中-公开
标题翻译：定位方法和装置
公开(公告)号：WO00047943A1
公开(公告)日：2000-08-17
申请号：PCT/EP2000/000276
申请日：2000-01-15
IPC分类号： F41G3/06 , F41G7/22 , G01S3/789 , G01S17/08
CPC分类号： F41G3/065 , F41G7/2226 , F41G7/2253 , F41G7/2293
摘要： The invention relates to a target detection method and a corresponding device (10). According to the invention, a target (2) is scanned in the course of a measurement by means of a distance measuring device (22) comprising a controllable detection area. During said measurement the dimensions of the target are identified on the basis of the sudden distance change at the edges (2a, 2b) of the target (2). The target-detection device (1) is immobile and the scanning motion is effected by deflecting the scanning beam (26) of the distance-measuring device (22).
摘要翻译：目标获取方法和装置（10），由具有可控制的检测范围，目标的测距仪（22）扫描（2）的测量，其中所述距离跳跃的边缘处的基础（2A，2B）的目标（2）的被检测出的目标的尺寸。目标检测装置（10）保持静止，并通过偏转测距仪（22）的探测光束（26）进行扫描移动。

25. 发明申请

WO9938033A8 GENERAL ASPHERE-CONIC CONFORMAL OPTICAL WINDOWS 审中-公开
标题翻译：一般的近似一致的光学窗口
公开(公告)号：WO9938033A8
公开(公告)日：1999-10-07
申请号：PCT/US9825911
申请日：1998-12-07
申请人： RAYTHEON CO
发明人： CROWTHER BLAKE G , MCKENNEY DEAN B , SPARROLD SCOTT W , MILLS JAMES B
IPC分类号： G01B11/24 , F41G7/22 , G01S7/48 , G02B27/00 , G02B
CPC分类号： F42B10/46 , F41G7/2253 , F41G7/2293
摘要： An optical system (26) includes a window (24) made of a curved piece of a transparent material having an inner surface (28) and an outer surface (30). The inner surface (28) has a nominal inner surface shape defined by a first conicoidal relationship, and the outer surface (30) has a nominal general aspheric surface shape. The optical system (26) also typically includes a sensor (32) and an optical train (36) on the side of the inner surface (28) of the window (24). The accuracy of the shape of the inner surface (28) is tested by directing a coherent light beam through a remote focus (54) of the inner surface (28), reflecting the light beam from the inner surface (28) toward an adjacent focus (52) of the inner surface (28), reflecting the light beam from a spherical reflector (60) at the adjacent focus (52) of the inner surface (28) and back toward the inner surface (28), reflecting the light beam from the inner surface (28) back toward the remote focus (54), and interferometrically comparing the reflected beam arriving at the remote focus (54) with a reference beam.
摘要翻译：一种光学系统（26）包括由具有内表面（28）和外表面（30）的透明材料的弯曲片制成的窗口（24）。内表面（28）具有由第一锥形关系限定的标称内表面形状，并且外表面（30）具有标称的普通非球面表面形状。光学系统（26）通常还包括窗口（24）的内表面（28）侧上的传感器（32）和光学系统（36）。通过将相干光束引导通过内表面（28）的远程焦点（54）来测试内表面（28）的形状的准确度，将来自内表面（28）的光束反射到相邻焦点（28）的内表面（52）上，将来自球形反射器（60）的光束反射到内表面（28）的相邻焦点（52）处并反射回内表面（28），反射光束从内表面（28）回到远程焦点（54），并干涉地比较到达远程焦点（54）的反射光束与参考光束。

26. 发明申请

WO99038033A2 GENERAL ASPHERE-CONIC CONFORMAL OPTICAL WINDOWS 审中-公开
标题翻译：一般的平方米一致的光学窗口
公开(公告)号：WO99038033A2
公开(公告)日：1999-07-29
申请号：PCT/US1998/025911
申请日：1998-12-07
IPC分类号： G01B11/24 , F41G7/22 , G01S7/48 , G02B27/00 , G02B
CPC分类号： F42B10/46 , F41G7/2253 , F41G7/2293
摘要： An optical system (26) includes a window (24) made of a curved piece of a transparent material having an inner surface (28) and an outer surface (30). The inner surface (28) has a nominal inner surface shape defined by a first conicoidal relationship, and the outer surface (30) has a nominal general aspheric surface shape. The optical system (26) also typically includes a sensor (32) and an optical train (36) on the side of the inner surface (28) of the window (24). The accuracy of the shape of the inner surface (28) is tested by directing a coherent light beam through a remote focus (54) of the inner surface (28), reflecting the light beam from the inner surface (28) toward an adjacent focus (52) of the inner surface (28), reflecting the light beam from a spherical reflector (60) at the adjacent focus (52) of the inner surface (28) and back toward the inner surface (28), reflecting the light beam from the inner surface (28) back toward the remote focus (54), and interferometrically comparing the reflected beam arriving at the remote focus (54) with a reference beam.
摘要翻译：光学系统（26）包括由具有内表面（28）和外表面（30）的透明材料的弯曲件制成的窗（24）。内表面（28）具有由第一锥形关系限定的标称内表面形状，并且外表面（30）具有标称的一般非球面形状。光学系统（26）通常还包括在窗口（24）的内表面（28）侧的传感器（32）和光学系统（36）。通过将相干光束引导通过内表面（28）的远焦点（54）来测试内表面（28）的形状的精度，将来自内表面（28）的光束反射到相邻焦点（28）的反射镜（52），反射来自内表面（28）的相邻焦点（52）处的球形反射器（60）的光束并且朝向内表面（28）反射，反射光束从内表面（28）返回到远焦点（54），并且将到达远焦点（54）的反射光束与参考光束进行干涉比较。

27. 发明申请

WO99018468A1 DYNAMIC OPTICAL CORRECTOR 审中-公开
标题翻译：动态光学校正器
公开(公告)号：WO99018468A1
公开(公告)日：1999-04-15
申请号：PCT/US1998/020897
申请日：1998-10-01
IPC分类号： F41G7/22 , G02B17/08 , G02B26/06 , G02B26/00 , F42B15/00
CPC分类号： G02B17/0884 , F41G7/2213 , F41G7/2253 , F41G7/2293 , G02B17/0808 , G02B17/0852 , G02B26/06
摘要： A programmable optical system (50) that dynamically corrects or induces aberrations into the optical path of a missile seeker. The system is dynamic in that the amount and type of aberration may be changed while the missile is in flight. The dynamic correction is accomplished by means of deformations applied to a low-mass mirror (80) or mirrors in the optical path of the missile seeker. The missile includes an aspheric dome (60), and the optical system is dynamically compensated for aberrations introduced by the dome as the seeker system is moved through the field of regard.
摘要翻译：一种可编程光学系统（50），其可动态地校正或诱导到导弹探测器的光路中的像差。该系统是动态的，因为导弹在飞行中可能会改变像差的数量和类型。通过施加到导弹探测器的光路中的低质量反射镜（80）或反射镜的变形来实现动态校正。该导弹包括一个非球面圆顶（60），并且当引导系统移动通过该领域时，光学系统被动态补偿由圆顶引入的像差。

28. 发明申请

WO1998023914A2 CONTROL SYSTEM FOR GUN AND ARTILLERY PROJECTILES 审中-公开
标题翻译：枪械和工艺品控制系统
公开(公告)号：WO1998023914A2
公开(公告)日：1998-06-04
申请号：PCT/US1997021582
申请日：1997-11-24
申请人： TRACOR AEROSPACE, INC.
发明人： TRACOR AEROSPACE, INC. , SALLEE, Bradley , SCHORR, David
IPC分类号： F41G07/22
CPC分类号： F41G7/226 , F41G7/222 , F41G7/2293 , F42B10/60
摘要： A directional control system for ballistic projectiles, including a projectile capable of being fired from a gun, a tracking device within the projectile capable of sensing and identifying a preferred target direction, a moveable mass located within the projectile, an electromagnetic mass-shifting device within the projectile capable of reversibly moving the mass from a first position to a second position whereby the flight path of the projectile is controlled. The directional control system may be used with a projectile which has no externally protruding bodies. The system includes at least one microprocessor programmed to obtain input from the tracking device and to perform calculations to determine movements of the mass. The moveable mass is positioned to shift the momentum vector perpendicular to the central longitudinal spin axis of the projectile when in motion. The mass shifting device preferably includes an electromagnetic driver, which is aligned such that the mass can be moved reversibly from a first position to a second position. The system preferably includes a tracking device including optical fibers for receiving incoming radiation. The system may include a tracking device which is sensitive to radio frequency radiation, and has at least one antenna sensitive to radio frequency radiation. The tracking device may alternatively have at least one infrared detector sensitive to infrared radiation, and preferably has a pyroelectric detector pair.
摘要翻译：一种用于弹道射弹的方向控制系统，包括能够从枪射出的射弹，能够感测和识别优选目标方向的射弹内的跟踪装置，位于射弹内的可移动质量块，电磁质量移动装置，该弹丸能够将质量从第一位置可逆地移动到第二位置，由此控制射弹的飞行路径。方向控制系统可以与没有外部突出体的射弹一起使用。该系统包括至少一个微处理器，其被编程以从跟踪装置获得输入并执行计算以确定质量的运动。可移动质量块定位成在运动时垂直于弹丸的中心纵向旋转轴线移动动量矢量。质量移动装置优选地包括电磁驱动器，其被对准使得质量可以从第一位置可逆地移动到第二位置。该系统优选地包括跟踪装置，其包括用于接收进入的辐射的光纤。该系统可以包括对射频辐射敏感的跟踪装置，并且具有对射频辐射敏感的至少一个天线。跟踪装置可替代地具有至少一个对红外辐射敏感的红外检测器，并且优选地具有热电检测器对。

29. 发明申请

WO1998016794A2 ONE-MAN AIR-DEFENCE GUIDED MISSILE 审中-公开
标题翻译：一人空中导向的MISSILE
公开(公告)号：WO1998016794A2
公开(公告)日：1998-04-23
申请号：PCT/RU1997000320
申请日：1997-10-10
申请人： KONSTRUKTORSKOE BJURO MASHINOSTROENYA
发明人： KONSTRUKTORSKOE BJURO MASHINOSTROENYA , GUSCHIN, Nikolai Ivanovich , FOKIN, Ruslan Vasilievich , DEEV, Leonid Georgievich , BATISCHEV, Konstantin Alexandrovich , SUDARIKOV, Valery Ivanovich , SMIRNOV, Alexandr Gennadievich , OGNEV, Vladimir Nikolaevich , VUKOLOV, Alexandr Sergeevich , YABLONSKY, Alexandr Sergeevich , KUVSHINOV, Alfei Mikhailovich , VOROBIEV, Viktor Evgenievich , ZHUKOV, Alexandr Pavlovich
IPC分类号： F41F00/00
CPC分类号： F42C13/02 , F41G7/007 , F41G7/2253 , F41G7/2293
摘要： The present invention pertains to the field of rocketry and relates to a guided missile that belongs to the category of portable air-defence devices and is intended for the interception of low-flying targets. The missile of the present invention comprises the following members: a self-guided thermal head comprising a detector for measuring the misalignment angle between the missile longitudinal axis and the optical axis of the thermal head co-ordinator (target bearing-angle detector); a solid-fuel drive unit comprising a dual-mode cruise engine as well as an acceleration engine fitted in the launch tube; an instrumental section comprising a flight-controls actuator, an onboard power unit as well as an onboard connector for switching the electrical circuits of the missile with the launch device before launching; an explosive and fragmentation offensive load comprising a rocket functional unit that generates a pulse for triggering the electric detonator of the offensive load; and a sensor for detecting the main vortex flow of the target as well as a backup target-impact detector. In order to increase the potential of target destruction, the offensive load body comprises a target non-contacting laser detector as well as a formatter of a tuneable delay for the offensive load firing pulse. The delay of the offensive load firing pulse is tuned by the person firing the missile using switches in the launch tube and in the launch device. The delay is also tuned using an automatic switch for selecting a tracking- or encounter-type interception mode thanks to the link between the control circuit of the delay formatter and the bearing detector of the self-guided thermal head. The moment when the offensive load is fired is determined according to the selected delay value while accounting for the target speed, trajectory and dimension as well as for the interception conditions thereof (tracking or encounter).
摘要翻译：本发明涉及火箭领域，涉及一种属于便携式防空装置类别的导弹，目的在于拦截低飞行目标。本发明的导弹包括以下构件：自导热头，其包括用于测量导热纵轴和热头协调器（目标支承角检测器）的光轴之间的未对准角度的检测器; 固体燃料驱动单元，包括双模式巡航发动机以及安装在发射管中的加速引擎; 仪器部分包括飞行控制致动器，车载动力单元以及用于在发射之前用发射装置切换导弹的电路的板载连接器; 一种爆炸性和破碎性的攻击性载荷，包括产生用于触发进攻性负载的电雷管的脉冲的火箭功能单元; 以及用于检测目标的主涡流的传感器以及备用目标撞击检测器。为了增加目标破坏的潜力，令人反感的负载体包括目标非接触式激光检测器以及用于进攻负载点火脉冲的可调节延迟格式器。射击负载发射脉冲的延迟是由发射管和发射装置中的开关使用发射导弹的人调整的。由于延迟格式器的控制电路和自引导热头的轴承检测器之间的联系，延迟也使用自动开关进行调谐，这种自动开关用于选择跟踪或遇到型截取模式。根据所选择的延迟值来确定进攻负载被触发的时刻，同时考虑目标速度，轨迹和尺寸以及其拦截条件（跟踪或遇到）。

30. 发明申请

WO1993001465A1 OPTICAL SYSTEM IN A LASER GUIDANCE SYSTEM 审中-公开
标题翻译：激光指导系统中的光学系统
公开(公告)号：WO1993001465A1
公开(公告)日：1993-01-21
申请号：PCT/US1992005602
申请日：1992-07-02
申请人： LTV MISSILES AND ELECTRONICS GROUP
发明人： LTV MISSILES AND ELECTRONICS GROUP , KRASUTSKY, Nicholas, J. , MINOR, Lewis, G. , FLOWERS, Edward, M.
IPC分类号： F41G07/22
CPC分类号： F41G7/2246 , F41G7/2213 , F41G7/2293 , G01S7/481 , G01S7/4817 , G01S7/484 , G01S17/10 , G02B27/106 , G02B27/108 , G02B27/1093 , G02B27/143 , G02B27/283
摘要： An apertured mirror permits an outgoing, transmitted laser beam to pass and reflects a return, reflected beam onto a detector array. A gimballed optical system within a seeker head inlcudes a relatively low power laser coupled to a relatively higher power laser by way of a flexible fiber optic cable to reduce the mass that must be oscillated in a scan. An optical device within the laser radar transmitter uses successive calcite wedges for segmenting the emitted beam into multiple, diverging beams which define a fan-shaped pattern of overlapping beams. The calcite wedges are arrayed coaxially along the optical path, and a series of 1/4 wave retarders are interposed between adjacent wedges to reestablish circular polarization.
摘要翻译：有孔镜允许输出的透射的激光束通过并将返回的反射光束反射到检测器阵列上。寻求者头部内的一个圆顶光学系统包括通过柔性光缆连接到相对较高功率的激光器的相对较低功率的激光器，以减少必须在扫描中振荡的质量。激光雷达发射器内的光学装置使用连续的方解石楔，将发射的光束分成多个发散光束，其限定重叠光束的扇形图案。方解石楔沿光路同轴排列，一系列1/4波延迟器置于相邻的楔块之间，以重新建立圆极化。

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