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1. 发明授权

US07503521B2 Radiation homing tag 有权
标题翻译：辐射归位标签
公开(公告)号：US07503521B2
公开(公告)日：2009-03-17
申请号：US11629061
申请日：2006-02-07
申请人： John A. Maynard , James M. Ortolf , Mark A. Carlson , Paul D. Zemany
发明人： John A. Maynard , James M. Ortolf , Mark A. Carlson , Paul D. Zemany
IPC分类号： F41G7/00 , G01S1/00 , F42B15/01 , G01S13/00 , F42B15/00
CPC分类号： F41G7/226 , F41G3/18 , F41G7/2293 , F42B12/365 , F42B12/40 , G01S1/70
摘要： The homing tag (1) has a transmissive housing (3), which is attached to a cartridge case (5). The transmissive housing (3) includes an aft body (7) to provide an interface with the cartridge case (5). Rotating bands (9) are located at a leading edge of the aft body (7). The transmissive housing (3) further includes a central body (11). The ogive-shaped nose (13) is formed of transparent material. A pluralit of slots (15) are provided for cooling the transmissive housing (3).
摘要翻译：归位标签（1）具有连接到盒壳体（5）的透射壳体（3）。透射壳体（3）包括一个后部主体（7），以提供与盒壳体（5）的接口。旋转带（9）位于后身（7）的前缘。透射壳体（3）还包括中心体（11）。原始形状的鼻子（13）由透明材料形成。多个槽（15）被设置用于冷却透射壳体（3）。

2. 发明授权

US07834300B2 Ballistic guidance control for munitions 有权
标题翻译：弹道导弹控制弹药
公开(公告)号：US07834300B2
公开(公告)日：2010-11-16
申请号：US11629060
申请日：2006-02-07
申请人： Paul D. Zemany , Mark A. Carlson , John A. Maynard
发明人： Paul D. Zemany , Mark A. Carlson , John A. Maynard
IPC分类号： F42B15/01 , F42B10/60 , F42B10/62 , F42B15/00 , F42B10/00
CPC分类号： F41G7/2293 , F41G7/222 , F41G7/226 , F42B10/06 , F42B10/64 , F42B15/01
摘要： A method and system for guiding and controlling an ordinance body having a trajectory and a bore sight angle including making corrections to the trajectory based on bore sight angle vs. time history. The system is incorporated with existing fuse components in a replacement kit for existing munitions. The method determines nominal time values of the ballistic trajectory of the munition in relation to launch time and determines deviation from the nominal time values by an algorithm by analyzing signals received from a source of radiation located at the target. A processor determines lateral (left/right) and range errors and provides commands to a plurality of flight control surfaces mounted on the munition.
摘要翻译：用于引导和控制具有轨迹和钻孔视角的条例体的方法和系统，包括基于钻孔视角对时间历史对轨迹进行校正。该系统与现有的弹药更换套件中的现有保险丝组件相结合。该方法确定弹药弹道轨迹与发射时间的标称时间值，并通过分析从位于目标位置的辐射源接收的信号，确定通过算法与标称时间值的偏差。处理器确定横向（左/右）和范围误差，并向安装在弹药上的多个飞行控制表面提供命令。

3. 发明授权

US07533849B2 Optically guided munition 有权
标题翻译：光导弹
公开(公告)号：US07533849B2
公开(公告)日：2009-05-19
申请号：US11629062
申请日：2006-02-07
申请人： Paul D. Zemany , Mark A. Carlson , John A. Maynard
发明人： Paul D. Zemany , Mark A. Carlson , John A. Maynard
IPC分类号： F41G7/00 , F42B15/01 , F42B15/00
CPC分类号： F41G7/226 , F41G7/222 , F41G7/2293 , F42B10/64 , F42B15/01
摘要： An optically guided mortar comprising a three axis canard assembly, an optical seeker, a guidance and control processor, and a fuze mechanism. The optical seeker is a direct replacement for existing standard mortar fuzes. The resulting system significantly improves current mortar circular error probability (CEP) and results in overall reduction of cost of target prosecution, reduction in collateral damage, improved crew survivability, and adds compatibility against limited non-stationary targets. The optical seeker detects an optical illuminator located at a target and supplies signals to the guidance and control processor which through a guidance algorithm supplies steering commands to drive motors of the three axis canard assembly which move a plurality of guidance canards to accurately direct the munition toward a target.
摘要翻译：一种光学引导的砂浆，其包括三轴组件，光学探针，引导和控制处理器以及引信机构。光学探测器直接替代现有的标准砂浆。所产生的系统显着改善了当前的迫击炮循环误差概率（CEP），并导致目标检测成本的总体降低，减少附带损害，提高了机组的生存能力，并增加了与有限非平稳目标的兼容性。光学探测器检测位于目标位置的光学照明器，并向引导和控制处理器提供信号，引导和控制处理器通过引导算法提供转向命令来驱动三轴卡车组件的马达，移动多个导向槽，以准确地将弹药导向一个目标。

4. 发明申请

US20090039197A1 Optically Guided Munition Control System and Method 有权
标题翻译：光导导弹控制系统与方法
公开(公告)号：US20090039197A1
公开(公告)日：2009-02-12
申请号：US11632671
申请日：2006-02-07
申请人： John A. Maynard , Mark A. Carlson , Paul D. Zemany
发明人： John A. Maynard , Mark A. Carlson , Paul D. Zemany
IPC分类号： F42B15/01
CPC分类号： F42B15/01 , F41G7/222 , F41G7/226 , F41G7/2293 , G05D1/12
摘要： An optically guided munition and control system has a replacement fuse assembly mounted on the front of a munition body or shell casing. An optical seeker subsystem detects an illuminated target and supplies signals to a processor. The processor develops steering commands sent to a flight control subsystem having a plurality of guidance canards which are actuated by drive motors through gear assemblies. The roll of the munition is established and left/right and up/down steering commands are sent to the canard drive motors based upon the optical seeker subsystem detection of the target illuminator. Range adjustment is based upon bore sight lockdown angle and cross range control is based upon left/right centering error. A code is contained in the optical radiation received from the illuminated target which must be validated by a preset code in the system processor to arm the munition.
摘要翻译：一个光学导弹的弹药和控制系统具有安装在弹药体或壳体外面的替换保险丝组件。光学探针子系统检测被照射的目标并向处理器提供信号。处理器开发发送到飞行控制子系统的转向命令，该飞行控制子系统具有由驱动马达通过齿轮组件驱动的多个导向槽。建立弹药卷，基于目标照明器的光学引导器子系统检测，左/右上下转向命令被发送到卡车驱动马达。范围调整基于钻孔视距锁定角度，并且跨距控制基于左/右对中误差。从被照射的目标接收到的光辐射中包含一个代码，该光辐射必须通过系统处理器中的预设代码进行验证以便弹药。

5. 发明授权

US08450668B2 Optically guided munition control system and method 有权
标题翻译：光导制导控制系统及方法
公开(公告)号：US08450668B2
公开(公告)日：2013-05-28
申请号：US11632671
申请日：2006-02-07
申请人： John A. Maynard , Mark A. Carlson , Paul D. Zemany
发明人： John A. Maynard , Mark A. Carlson , Paul D. Zemany
IPC分类号： F42B15/01 , F42B10/62 , F42B15/00 , F42B10/00
CPC分类号： F42B15/01 , F41G7/222 , F41G7/226 , F41G7/2293 , G05D1/12
摘要： An optically guided munition and control system has a replacement fuse assembly mounted on the front of a munition body or shell casing. An optical seeker subsystem detects an illuminated target and supplies signals to a processor. The processor develops steering commands sent to a flight control subsystem having a plurality of guidance canards which are actuated by drive motors through gear assemblies. The roll of the munition is established and left/right and up/down steering commands are sent to the canard drive motors based upon the optical seeker subsystem detection of the target illuminator. Range adjustment is based upon bore sight lockdown angle and cross range control is based upon left/right centering error. A code is contained in the optical radiation received from the illuminated target which must be validated by a preset code in the system processor to arm the munition.
摘要翻译：一个光学导弹的弹药和控制系统具有安装在弹药体或壳体外面的替换保险丝组件。光学探针子系统检测被照射的目标并向处理器提供信号。处理器开发发送到飞行控制子系统的转向命令，该飞行控制子系统具有由驱动马达通过齿轮组件驱动的多个导向槽。建立弹药卷，基于目标照明器的光学引导器子系统检测，左/右上下转向命令被发送到卡车驱动马达。范围调整基于钻孔视距锁定角度，并且跨距控制基于左/右对中误差。从被照射的目标接收到的光辐射中包含一个代码，该光辐射必须通过系统处理器中的预设代码进行验证以便弹药。

6. 发明申请

US20160182013A1 TUNABLE EVANESCENT-MODE CAVITY FILTER WITH CLOSED LOOP CONTROL 有权
标题翻译：具有闭环控制的可逆过滤模式空气过滤器
公开(公告)号：US20160182013A1
公开(公告)日：2016-06-23
申请号：US14974324
申请日：2015-12-18
申请人： Thomas J. Johnson , Jack Chuang , Dimitrios Peroulis , Eric Naglich , Souleymane Gnanou , Curtis M. Grens , Mark Hickle , Michael D. Sinanis , Mark E. Stuenkel , Paul D. Zemany
发明人： Thomas J. Johnson , Jack Chuang , Dimitrios Peroulis , Eric Naglich , Souleymane Gnanou , Curtis M. Grens , Mark Hickle , Michael D. Sinanis , Mark E. Stuenkel , Paul D. Zemany
IPC分类号： H04B3/04 , H01P1/20
CPC分类号： H01P1/219 , H01P7/065 , H03J3/04 , H03J3/20
摘要： An evanescent-mode cavity filter with an improved MEMS tuner design is disclosed. The MEMS tuner design allows for the independent control of individual poles in a multi-pole filter, which increases the adaptability of the filter in a crowded RF environment. The filter is further designed to minimize tuning voltages and hysteresis effects. A closed loop control system provides highly responsive tuning of the filter. The closed loop control allows for accurate and stable tuning that compensates for temperature and vibrational effects, while the tuner design enables fast tuning and significantly increases the resolution of the feedback measurement by eliminating charge buildup in the tuner substrate.
摘要翻译：公开了一种具有改进的MEMS调谐器设计的ev逝模式空腔滤波器。 MEMS调谐器设计允许独立控制多极滤波器中的各个极，这增加了在拥挤的RF环境中滤波器的适应性。该滤波器进一步设计用于最小化调谐电压和滞后效应。闭环控制系统提供过滤器的高响应性调谐。闭环控制允许精确和稳定的调谐，补偿温度和振动效应，而调谐器设计可以快速调谐，并通过消除调谐器基板中的电荷积累，显着提高反馈测量的分辨率。

7. 发明授权

US08132491B2 Method and apparatus for detecting and disabling optical weapon sight 有权
标题翻译：用于检测和禁用光学武器瞄准器的方法和装置
公开(公告)号：US08132491B2
公开(公告)日：2012-03-13
申请号：US11451114
申请日：2006-06-12
申请人： Edward C. Real , Paul D. Zemany , Paul A. Zank
发明人： Edward C. Real , Paul D. Zemany , Paul A. Zank
IPC分类号： B64D1/04
CPC分类号： F41H13/0056
摘要： The present invention is an apparatus for detecting and disabling a human eye or optical device used in the fire control of a weapon. This apparatus comprises a prism having a plurality of peripheral reflective surface. This prism has a longitudinal axis and rotating about said longitudinal axis. An infrared (IR) laser directs an infrared laser beam toward the prism side that the laser beam is reflected toward the human eye or optical device, such that the IR laser beam is retroreflected to the prism. There is also an infrared IR detector which detects the IR retroreflected laser beam reflected from the prism. A visible light wavelength laser which produces a visible light wavelength laser beam which is reflected from the prism to the human eye or optical device to disable the human eye or optical device to prevent use of the weapon.
摘要翻译：本发明是一种用于检测和禁用在武器的火控中使用的人眼或光学装置的装置。该装置包括具有多个外围反射表面的棱镜。该棱镜具有纵向轴线并围绕所述纵向轴线旋转。红外（IR）激光器将红外激光束引导到棱镜侧，激光束朝向人眼或光学装置反射，使得IR激光束向后反射到棱镜。还有一个红外IR检测器，它检测从棱镜反射的红外回射激光束。一种可见光波长激光器，其产生从棱镜反射到人眼或光学装置的可见光波长激光束，以禁止人眼或光学装置阻止使用武器。

8. 发明授权

US07355545B2 Through the wall ranging with triangulation using multiple spaced apart radars 有权
标题翻译：通过使用多个间隔开的雷达进行三角测量的墙壁
公开(公告)号：US07355545B2
公开(公告)日：2008-04-08
申请号：US11121787
申请日：2005-05-03
申请人： Paul D. Zemany , Eldon M. Sutphin
发明人： Paul D. Zemany , Eldon M. Sutphin
IPC分类号： G01S13/00 , G01S17/10
CPC分类号： G01S13/888 , G01S13/003 , G01S13/584
摘要： A plurality of multi-tone CW radars are used to generate a swath of ranges to a moving object or individual behind a wall or building structure in which the overlap of the range swaths from spaced-apart radars determines the location of the moving object or individual. A histogram of the swath overlaps is used to generate a display of the path of the moving object or individual.
摘要翻译：使用多个多音调CW雷达来产生一幅范围的范围，该距离范围到墙壁或建筑结构后面的移动物体或个体，其中范围的重叠从间隔开的雷达确定移动物体或个体的位置。使用条带重叠的直方图来生成移动对象或个体的路径的显示。

9. 发明授权

US4791573A State-deviation-estimation circuit employing a phase-locked-loop phase reference 失效
标题翻译：采用锁相环相位参考的状态偏差估计电路
公开(公告)号：US4791573A
公开(公告)日：1988-12-13
申请号：US902815
申请日：1986-09-02
申请人： Paul D. Zemany , Kirby A. Smith , John A. Smith
发明人： Paul D. Zemany , Kirby A. Smith , John A. Smith
IPC分类号： G05D1/10 , G05D1/08 , B64G1/28 , B64G1/36
CPC分类号： G05D1/108
摘要： A system (34) for determining deviations in the state of motion of a projectile (10) from its intended state includes a comparison module (38) that receives the outputs S of a sensor array (36). The comparison module (38) converts the sensor outputs to a measurement vector Z.sub.m and computes the deviation of this measurement vector from an intended measurement vector Z.sub.0 received from a control system. The comparison module (38) then determines the difference E.sub.Z between this measured deviation and the deviation predicted by a Kalman filter (44, 46). In generating the measurement vector Z.sub.m from the outputs of the sensor array (36), the comparison module (38) "de-spins" the array outputs in accordance with the output of a phase reference (42), whose purpose is to indicate the phase with respect to gravity of the spin of the projectile (10) about its longitudinal axis. The Kalman filter's state-deviation estimator (46) weights the vector output of the comparison module (36) and adds it to the output of the Kalman filter's state-deviation predictor (44) to provide an updated state-deviation estimation E.sub.X (t:t), which the state-deviation predictor (44) then uses as a basis for its next cycle. The output of the comparison module (38) constitutes a measure of the performance of the state-deviation predictor (44) and is used as a correction factor for the phase reference (42) so that the system acts as a phase-locked loop to lock the phase reference (42) onto the projectile spin without the need for an external sensor to determine the direction of gravity.
摘要翻译：用于确定弹丸（10）的运动状态与其预期状态的偏差的系统（34）包括：接收传感器阵列（36）的输出S的比较模块（38）。比较模块（38）将传感器输出转换为测量矢量Zm，并计算该测量矢量与从控制系统接收到的预期测量矢量Z0的偏差。比较模块（38）然后确定该测量的偏差与由卡尔曼滤波器（44,46）预测的偏差之间的差EZ。在从传感器阵列（36）的输出生成测量矢量Zm时，比较模块（38）根据相位基准（42）的输出“去”旋转阵列输出，其目的是指示相对于射弹（10）的旋转的重力围绕其纵向轴线。卡尔曼滤波器的状态偏差估计器（46）对比较模块（36）的矢量输出进行加权，并将其加到卡尔曼滤波器的状态偏差预测器（44）的输出端，以提供更新的状态偏差估计EX（t： t），状态偏差预测器（44）然后用作其下一个周期的基础。比较模块（38）的输出构成了状态偏差预测器（44）的性能的量度，并被用作相位参考（42）的校正因子，使得系统充当锁相环将相位基准（42）锁定在抛射体旋转上，而不需要外部传感器来确定重力方向。

10. 发明授权

US07852256B2 Through the-wall motion detector with improved antenna 有权
标题翻译：通过改进天线的墙体运动检测器
公开(公告)号：US07852256B2
公开(公告)日：2010-12-14
申请号：US11919269
申请日：2006-10-11
申请人： Paul D. Zemany
发明人： Paul D. Zemany
IPC分类号： G01S13/04 , G01S13/88 , G01S7/02 , G01S13/00 , G01S13/89
CPC分类号： H01Q21/065 , G01S13/56 , G01S13/888 , H01Q1/1221 , H01Q1/22 , H01Q1/40
摘要： A flat panel antenna used at a wall in a through-the-wall CW radar application is spaced from the wall by a half wavelength to eliminate the effects of energy reflected by the wall back to the antenna. In one embodiment, a ½-wavelength dielectric absorbing material insert is placed adjacent the flat panel antenna, which allows the flat panel antenna to be pressed against the wall for antenna stabilization, with the index of refraction of the material desirably being 3.
摘要翻译：在通过墙壁CW雷达应用的墙壁处使用的平板天线与墙壁隔开半波长，以消除由壁反射回天线的能量的影响。在一个实施例中，½波长电介质吸收材料插入件被放置在平板天线附近，这允许平板天线被压靠在壁上用于天线稳定，其中材料的折射率理想地为3。

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