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1. 发明申请

WO2021154355A2 DUAL MODE SEMI-ACTIVE LASER SEEKER AND IMAGING SYSTEM 审中-公开
公开(公告)号：WO2021154355A2
公开(公告)日：2021-08-05
申请号：PCT/US2020/057489
申请日：2020-10-27
申请人： BAE SYSTEMS INFORMATION AND ELECTRONIC SYSTEMS INTEGRATION INC.
发明人： FREY, Robert D., Jr.
IPC分类号： F42B15/01 , G01S17/66 , G01S3/783 , G01S3/784 , G01S17/02 , F41G3/14 , F41G7/00 , F41G7/22 , F41G7/26 , G06T7/33
摘要： The system and method of a dual mode semi active laser seeker and imaging system using pulse detection and angle determination as applied to quad detectors to properly identify a correct designator spot. The angle performance is driven by the field of view of the imaging system. The imaging system resolution provides the required angle accuracy for guidance as cued by pulse detection apertures. The imaging system eliminates the need to designate until impact thus eliminating exposure to counter fire against the designator. The elimination of designation until impact also opens up the opportunity rapid engagement of multiple targets from a single designator.

2. 发明申请

WO2021091599A1 SUPER-RESOLUTION AUTOMATIC TARGET AIMPOINT RECOGNITION AND TRACKING 审中-公开
公开(公告)号：WO2021091599A1
公开(公告)日：2021-05-14
申请号：PCT/US2020/040571
申请日：2020-07-01
申请人： RAYTHEON COMPANY
发明人： BRAUNREITER, Dennis C.
IPC分类号： F41H13/00 , F41G3/14 , G06T7/246 , G06T3/40 , F41G5/08 , F42B15/01
摘要： A system includes at least one imaging sensor (228, 378) configured to capture images of a target (104). The system also includes at least one controller (230) configured to generate super-resolution images of the target using the captured images and identify multiple edges of the target using the super-resolution images. The at least one controller is also configured to identify an aimpoint on the target based on the identified edges of the target. In addition, the at least one controller is configured to update the aimpoint on the target as the target moves over time. The system may further include a high-energy laser (HEL) (202, 302) configured to generate an HEL beam (106) that is directed towards the target, and the at least one controller may be configured to adjust one or more optical devices (218, 220, 224, 342, 348, 354, 364) to direct the HEL beam at the identified aimpoint on the target.

3. 发明申请

WO2016130191A1 GUN-LAUNCHED BALLISTICALLY-STABLE SPINNING LASER-GUIDED MUNITION 审中-公开
标题翻译： GUN-LUNCHED BALLISTICTIC-STABLE SPINNING LASER-GUIDED MUNITION
公开(公告)号：WO2016130191A1
公开(公告)日：2016-08-18
申请号：PCT/US2015/062114
申请日：2015-11-23
申请人： RAYTHEON COMPANY
发明人： TRAIL, Nicholas, D.
IPC分类号： F42B10/66 , F42B15/01 , F41F1/00 , F41G7/22 , F42B10/26 , F41F1/10
CPC分类号： G05B15/02 , F41F1/00 , F41F1/10 , F41G7/222 , F41G7/226 , F41G7/2293 , F42B5/02 , F42B10/26 , F42B10/661 , F42B15/01
摘要： A gun-launched ballistically-stable spinning laser-guided munition comprises a plurality of explosive divert elements arranged around the bullet to produce a force vector through the center of mass (Cm) of the bullet, a SAL guidance system configured to measure a sequence of roll and nod angle pairs (or their equivalent) to the target, a processor configured to process the roll and nod angles to compute a firing solution for one or more of the divert elements to produce a force vector to laterally displace the bullet to drive the nod angle to a prescribed value and a fire controller configured, once its operational mode is initiated, to fire the one or more explosive divert elements according to the firing solution to laterally displace the bullet without affecting the bullet's angle of attack and destabilizing the bullet.
摘要翻译：枪支发射的弹道稳定的旋转激光制导弹药包括围绕子弹布置的多个爆炸转移元件，以产生通过子弹的质心（Cm）的力矢量; SAL引导系统，被配置成测量一系列滚动和点头对（或其等价物）到目标的处理器，处理器被配置为处理卷轴和点角度以计算一个或多个转向元件的点火解决方案，以产生向量以横向移位子弹以驱动将点火角设定为规定值，并设置防火控制器，一旦启动其操作模式，就可以根据点火解决方案对一个或多个爆炸转向元件进行点火，以横向移位子弹，而不会影响子弹的冲击力并使子弹不稳定。

4. 发明申请

WO2016067011A1 INERTIAL NAVIGATION SYSTEM WITH COMPENSATION OF ROLL SCALE FACTOR ERROR 审中-公开
标题翻译：惯性导航系统与滚动规模因子误差的补偿
公开(公告)号：WO2016067011A1
公开(公告)日：2016-05-06
申请号：PCT/GB2015/053216
申请日：2015-10-27
申请人： ATLANTIC INERTIAL SYSTEMS LIMITED
发明人： SHEARD, John Keith , FAULKNER, Nicholas Mark
IPC分类号： G01C21/16 , G01C25/00 , F41G7/36 , F42B15/01 , G05D1/10
CPC分类号： G01C21/16 , F41G7/36 , F42B15/01 , G01C25/005
摘要： An inertial measurement system (200) for a longitudinal projectile, comprising a first, roll gyro to be oriented substantially parallel to the longitudinal axis of the projectile; a second gyro and a third gyro with axes arranged with respect to the roll gyro such that they define a three dimensional coordinate system. The system further comprises a controller (225, 250), arranged: - to compute a current projectile attitude from the outputs of the first, second and third gyros, the computed attitude comprising a roll angle, a pitch angle and a yaw angle; - for at least two time points, to compare the computed pitch and yaw angles with expected values for the pitch and yaw angles; - for each of said at least two time points, to calculate a roll angle error based on the difference between the computed pitch and yaw angles and the expected pitch and yaw angles; - to calculate a roll angle error difference between said at least two time points; - to calculate the total roll angle subtended between said at least two time points; - to calculate a roll angle scale factor error based on said computed roll angle error difference and said total subtended roll angle and apply the calculated roll angle scale factor error to the output of the roll gyro.
摘要翻译：一种用于纵向抛射体的惯性测量系统（200），包括：基本上平行于射弹的纵向轴线定向的第一滚动陀螺仪; 具有相对于滚动陀螺仪布置的轴的第二陀螺仪和第三陀螺仪，使得它们限定三维坐标系。该系统还包括控制器（225,250），其被布置为： - 从所述第一，第二和第三陀螺仪的输出计算当前的射弹姿态，所述计算出的姿势包括侧倾角，俯仰角和偏航角; - 对于至少两个时间点，将计算的俯仰角和偏航角与俯仰角和偏航角的预期值进行比较; - 对于所述至少两个时间点中的每一个，基于所计算的俯仰角和偏航角与预期俯仰角和偏航角之间的差来计算侧倾角误差; - 计算所述至少两个时间点之间的侧倾角误差; - 计算所述至少两个时间点之间对准的总滚动角度; - 基于所述计算的侧倾角误差差和所述总对角侧倾角来计算滚转角缩放因子误差，并将所计算的滚转角缩放因子误差应用于滚动陀螺仪的输出。

5. 发明申请

WO2014074212A1 ROCKET PROPELLED PAYLOAD WITH DIVERT CONTROL SYSTEM WITHIN NOSE CONE 审中-公开
标题翻译：带诺斯锥内的DIVERT控制系统的ROCKET PROPLEED PAYLOAD
公开(公告)号：WO2014074212A1
公开(公告)日：2014-05-15
申请号：PCT/US2013/057771
申请日：2013-09-03
申请人： RAYTHEON COMPANY
发明人： FACCIANO, Andrew B. , ALKEMA, Michael S. , MOORE, Robert T.
IPC分类号： F42B15/01
CPC分类号： F42B10/663
摘要： A rocket is provided and includes booster stages at a rear of the nose cone, the booster stages being configured for propelling the nose cone in a propulsion direction and a divert control system housed entirely in the nose cone for controlling an orientation of the propulsion direction.
摘要翻译：提供火箭并且包括位于鼻锥后部的增压器级，增压级构造成用于沿推进方向推进鼻锥，而转向控制系统完全容纳在鼻锥中，用于控制推进方向的取向。

6. 发明申请

WO2013176595A1 AUTONOMOUS MEASUREMENT OF THE INITIAL VELOCITY OF AN OBJECT THAT CAN BE FIRED 审中-公开
标题翻译：自动测量可以启动的对象的初始速度
公开(公告)号：WO2013176595A1
公开(公告)日：2013-11-28
申请号：PCT/SE2013/000072
申请日：2013-05-15
申请人： BAE SYSTEMS BOFORS AB
发明人： FOHRMAN, Erik , HOLM, Tony
IPC分类号： G01C21/10 , F41G7/36 , F42B15/01 , G01P15/12
CPC分类号： G01P3/665 , F41A21/32 , F41G3/12 , F42B30/006 , G01P3/44 , G01P7/00 , G01P15/0888 , G01P15/12
摘要： The invention concerns a process for measuring the initial velocity V 0 of an object that can be fired such as a shell or projectile that exits a barrel, said measurement being based on measurement of the force exerted on a sensor device (100) configured inside the object that can be fired, characterized in that the force is measured autonomously inside the object by detection of changes in shape of the sensor device (100) during movement of said object inside the barrel prior to its exit. The invention also concerns a device for measuring the initial velocity V 0 of an object that can be fired such as a shell or projectile that exits the barrel of a firing device such as an artillery piece, comprising a force-detecting sensor device (100) configured inside the object that can be fired, characterized in that the force-detecting sensor device (100) is configured so as to detect changes in shape of said sensor device (100) during movement of said object inside the barrel prior to its exit, and in that an included signal-processing unit calculates and determines the initial velocity V 0 based on the detected changes in shape. The invention also concerns a device and process for measuring the acceleration forces acting on an object that can be fired during movement of said object inside the barrel prior to its exit.
摘要翻译：本发明涉及一种用于测量能够被击发的物体的初始速度V0的过程，例如壳体或离开枪管的射弹，所述测量是基于施加在配置在物体内部的传感器装置（100）上的力的测量其特征在于，通过在所述物体在其出口之前的所述物体在所述桶内移动期间检测所述传感器装置（100）的形状变化，在所述物体内自主测量所述力。本发明还涉及一种用于测量能够被击发的物体的初始速度V0的装置，所述初始速度V 0包括离开诸如火炮的击发装置的枪管的外壳或射弹，该装置包括：力检测传感器装置（100），其配置在能够被击发的物体内部，其特征在于，所述力检测传感器装置（100）被配置为在所述物体在其出口之前的所述物体的运动期间检测所述传感器装置（100）的形状变化，以及因为所包括的信号处理单元基于检测到的形状变化来计算并确定初始速度V0。本发明还涉及一种用于测量作用在物体上的加速力的装置和方法，所述加速度在所述物体在其出口之前在所述桶内运动期间可以被点燃。

7. 发明申请

WO2010011245A9 MULTI-CALIBER FUZE KIT AND METHODS FOR SAME 审中-公开
公开(公告)号：WO2010011245A9
公开(公告)日：2010-01-28
申请号：PCT/US2009/003109
申请日：2009-05-20
申请人： RAYTHEON COMPANY , GESWENDER, Chris, E. , SANCHEZ, Cesar , ZAMORA, Matthew A.
发明人： GESWENDER, Chris, E. , SANCHEZ, Cesar , ZAMORA, Matthew A.
IPC分类号： F42B15/01
摘要： A multi-caliber fuze kit includes a fuze housing configured for coupling with multiple projectiles. One or more canards are moveably coupled with the fuze housing. The one or more canards are adjustable between two or more canard configurations. In a first canard configuration, the one or more canards are at a first canard angle relative to a bore sight of the fuze housing, and the first canard angle is configured for use with a first projectile. In a second canard configuration, the one or more canards are at a second canard angle relative to the bore sight of the fuze housing, and the second canard angle is configured for use with a second projectile. The first and second canard angles are different.

8. 发明申请

WO2008121431A2 MUNITIONS CONTROL UNIT 审中-公开
标题翻译：机组控制单元
公开(公告)号：WO2008121431A2
公开(公告)日：2008-10-09
申请号：PCT/US2008052295
申请日：2008-01-29
申请人： RAYTHEON CO , SITZMANN RICHARD L , PETERS RYAN J , HAGGH ALAN
发明人： SITZMANN RICHARD L , PETERS RYAN J , HAGGH ALAN
IPC分类号： F42B15/01 , F41F3/06 , F41G7/00
CPC分类号： F41F3/06 , F41F3/055 , F41G7/007
摘要： A munitions control unit (30) for integrating existing electronics of a vehicle (10) with at least one weapon (22), wherein said existing vehicle electronics are not equipped to interface with the at least one weapon includes a first I/O interface (32) for communicating control signals with said vehicle (10), at least one second I/O interface (34a-34d, 35a-35b, 37) different from the first I/O interface (32), said at least one second I/O interface communicating control signals with said weapon (22), a processor (57) and memory (58) operatively coupled to said first and at least one second I/O interface, and reconfigurable logic stored in memory and executable by the processor. The reconfigurable logic is operative to enable the munitions control unit to interface with a plurality of vehicles having different interfaces.
摘要翻译：一种用于将车辆（10）的现有电子装置与至少一个武器（22）集成的弹药控制单元（30），其中所述现有车辆电子设备未配备与所述至少一个武器的接口包括第一I / O接口 32），用于与所述车辆（10）通信控制信号，不同于所述第一I / O接口（32）的至少一个第二I / O接口（34a-34d，35a-35b，37），所述至少一个第二I / O接口与所述武器（22）通信控制信号，可操作地耦合到所述第一和至少一个第二I / O接口的处理器（57）和存储器（58）以及存储在存储器中并由处理器执行的可重配置逻辑。可重构逻辑可操作以使得弹药控制单元与具有不同接口的多个车辆相接合。

9. 发明申请

WO2008102069A2 GUIDED MISSILE WITH A SLEEVE FOR MOUNTING A GUIDING SYSTEM 审中-公开
标题翻译：引导与指示系统安装的套管
公开(公告)号：WO2008102069A2
公开(公告)日：2008-08-28
申请号：PCT/FR2007002142
申请日：2007-12-20
申请人： ATELIERS MECANIQUES DE PONT SU , MARTIN CHRISTIAN
发明人： MARTIN CHRISTIAN
IPC分类号： F42B15/01
CPC分类号： F42B15/01
摘要： The invention relates to a guided missile (1) comprising: a body (10) with a generally cylindrical shape ending at the front in a cone-shaped nose (20); and a cylindrical sleeve (30) for mounting a NATO-standard guiding system at the front of the body; characterised in that the nose (20) includes a cylindrical connection portion (25) on which the sleeve (30) is attached.
摘要翻译：本发明涉及一种导弹（1），包括：主体（10），其具有大致圆柱形的形状，其终端于锥形鼻（20）的前部; 以及用于在身体前部安装北约标准导向系统的圆柱形套筒（30）其特征在于，所述鼻部（20）包括圆柱形连接部分（25），所述套筒（30）附接在所述圆柱形连接部分上。

10. 发明申请

WO2007044922A3 METHODS AND APPARATUS FOR GUIDANCE SYSTEMS 审中-公开
标题翻译：指导系统的方法和装置
公开(公告)号：WO2007044922A3
公开(公告)日：2007-09-27
申请号：PCT/US2006040194
申请日：2006-10-13
申请人： RAYTHEON CO , JENKINS DAVID G , TAYLOR BYRON B
发明人： JENKINS DAVID G , TAYLOR BYRON B
IPC分类号： F41G7/00 , F42B15/01
CPC分类号： F41G7/226 , F41G7/2293 , G01S3/781 , G01S3/784 , G02B5/00 , G02B19/0014 , G02B19/0028 , G02B19/0076
摘要： The optical system comprises a condenser (420) and a spreader (415) The spreader (415) subdivides an input aperture of the optical system into subregions The condenser (420) condenses the energy transmitted by the spreader (415) onto a detector Subdividing the aperture tends to minimize the effects of fluctuations larger than the size of the subregions on the transfer function.
摘要翻译：所述光学系统包括冷凝器（420）和扩散器（415）。所述扩展器（415）将所述光学系统的输入孔细分成子区域。所述冷凝器（420）将由所述扩展器（415）传输的能量冷凝到检测器上孔径倾向于最小化波动大于分区域尺寸对传递函数的影响。

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