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101. 发明授权

US09518807B2 Projectile control systems and methods 有权
标题翻译：射弹控制系统和方法
公开(公告)号：US09518807B2
公开(公告)日：2016-12-13
申请号：US14333088
申请日：2014-07-16
申请人： Rosemount Aerospace Inc.
发明人： Gregory Nash , Gary Willenbring , Robert L. Alford
IPC分类号： F42B15/01 , F42B10/62 , G05D1/08 , G05D1/10 , F42B15/00 , F42B10/00
CPC分类号： F42B15/01 , F42B10/62 , G05D1/0816 , G05D1/107
摘要： A method of controlling a projectile includes initiating an execution mode if a roll control authority parameter is outside of a pre-determined operating range for a projectile. The execution mode includes bypassing a guidance command and sending a modified command to execute a coning maneuver to improve control response of the projectile. A projectile control system includes a processor operatively connected to a memory. The memory has instructions recorded thereon that, when read by the processor, cause the processor to execute the method operations described above.
摘要翻译：控制射弹的方法包括：如果滚动控制权限参数在射弹的预定操作范围之外，则启动执行模式。执行模式包括绕过引导命令并发送修改的命令以执行锥形操纵以改善射弹的控制响应。射弹控制系统包括可操作地连接到存储器的处理器。存储器具有记录在其上的指令，当由处理器读取时，使处理器执行上述方法操作。

102. 发明申请

US20160195878A1 MISSILE SYSTEM WITH NAVIGATION CAPABILITY BASED ON IMAGE PROCESSING 审中-公开
标题翻译：基于图像处理的导航能力的MISSILE系统
公开(公告)号：US20160195878A1
公开(公告)日：2016-07-07
申请号：US14911469
申请日：2014-06-15
申请人： RAFAEL ADVANCED DEFENSE SYSTEMS LTD
发明人： Omri PELEG , Eran SHIMONOVITZ , Avfram LEVY
IPC分类号： G05D1/10 , F41G7/34 , G05D1/00 , F42B15/01 , F41G7/22
CPC分类号： G05D1/107 , F41G7/007 , F41G7/008 , F41G7/2206 , F41G7/2213 , F41G7/2253 , F41G7/2293 , F41G7/30 , F41G7/343 , F42B15/01 , G01C21/12 , G01S5/16 , G05D1/0038
摘要： The present invention relates to electro-optic guided missile systems and, in particular, it concerns systems and methods providing enhanced navigation capabilities based on ego-motion processing of seeker images. The missile system comprising: a missile; a seeker located at a nose portion of said missile, said seeker comprising an electro-optic imaging sensor; and a control arrangement for steering the missile along a flight path to a target, characterized in that the missile system further comprises: a navigation subsystem receiving images from said imaging sensor, said navigation subsystem being configured to: co-process a plurality of said images from said imaging sensor to derive ego-motion of said missile relative to a region viewed by said imaging sensor; derive from said ego-motion a calculated target direction from said missile to a target.
摘要翻译：本发明涉及电光导弹系统，特别涉及提供基于探测器图像的自动运动处理的增强导航能力的系统和方法。导弹系统包括：导弹; 位于所述导弹的鼻部的探测器，所述探测器包括电光成像传感器; 以及用于将导弹沿着飞行路径转向目标的控制装置，其特征在于，所述导弹系统还包括：导航子系统，从所述成像传感器接收图像，所述导航子系统被配置为：协同处理多个所述图像从所述成像传感器导出所述导弹相对于由所述成像传感器观看的区域的自身运动; 从所述自我运动导出从所述导弹到目标的计算目标方向。

103. 发明申请

US20160138893A1 REMOTELY GUIDED GUN-FIRED AND MORTAR ROUNDS 有权
标题翻译：远程导向的枪和火箭圈
公开(公告)号：US20160138893A1
公开(公告)日：2016-05-19
申请号：US14225358
申请日：2014-03-25
申请人： Jahangir S. Rastegar
发明人： Jahangir S. Rastegar
IPC分类号： F41G7/30 , G06T7/00 , G05D1/12 , F42B15/01
CPC分类号： F41G7/30 , F41G7/306 , F42B12/365 , F42B15/01 , F42B30/006 , F42B30/10 , G05D1/0038 , G05D1/107 , G05D1/12 , G06T2207/20101
摘要： A method for guiding a gun-fired or mortared round towards an intended target. The method including: capturing image data from an image pick-up device during a descent of the round; transmitting the image data to a control platform remotely located from the round; receiving the image date at the control platform; displaying the image data to a user at the control platform; manually identifying one or more features in the image data on the monitor; and stabilizing the image on the monitor based on the one or more identified features.
摘要翻译：一种用于向预期目标引导炮击或迫击炮弹的方法。该方法包括：在下降期间从图像拾取装置捕获图像数据; 将图像数据发送到远离该圆的远程控制平台; 在控制平台上接收图像日期; 在控制平台上向用户显示图像数据; 手动识别监视器上的图像数据中的一个或多个特征; 以及基于所述一个或多个所识别的特征来稳定所述监视器上的图像。

104. 发明申请

US20160097621A1 MULTI-HYPOTHESIS FIRE CONTROL AND GUIDANCE 审中-公开
标题翻译：多发性火灾控制与指导
公开(公告)号：US20160097621A1
公开(公告)日：2016-04-07
申请号：US14876306
申请日：2015-10-06
申请人： The Charles Stark Draper Laboratory, Inc.
发明人： Tom P. Bucklaew , Christopher M. Gibson
IPC分类号： F42B15/01 , G05D1/10
CPC分类号： F42B15/01 , G05D1/107 , G05D1/12
摘要： This disclosure provides systems, methods, and apparatus for intercepting a moving target by a plurality of interceptors that individually have insufficient capability to achieve intercept. An electronic processor can receive information corresponding to a state of the moving target at a first time. The electronic processor can determine a plurality of hypotheses for the future maneuvers of the moving target. The hypotheses can be based in part on the state of the moving target at the first time and the location of any defended assets. The electronic processor can assign a respective target maneuver hypothesis or set of hypotheses to each of a plurality of interceptors. The electronic processor can assign firing times and/or initial guidance commands to each interceptor. The electronic processor can update the set of feasible hypotheses based on additional receipt of information on the motion of the target and communicate this information to interceptors in flight via a communication subsystem. The electronic processor, or a secondary electronic processor located on each interceptor, can control each interceptor to maneuver such that the moving target is intercepted, based on the respective target maneuver hypotheses.
摘要翻译：本公开提供了用于通过单独具有不足以实现截距的能力的多个拦截器拦截移动目标的系统，方法和装置。电子处理器可以在第一时间接收与移动目标的状态相对应的信息。电子处理器可以确定用于移动目标的未来机动的多个假设。这些假设可以部分地基于第一次移动目标的状态和任何被辩护资产的位置。电子处理器可以为多个拦截器中的每一个分配相应的目标操纵假设或一组假设。电子处理器可以向每个拦截器分配发射时间和/或初始指导命令。电子处理器可以基于关于目标运动的信息的额外接收来更新该组可行假设，并将该信息通过通信子系统传送给飞行中的拦截器。位于每个拦截器上的电子处理器或次级电子处理器可以基于相应的目标操纵假设来控制每个拦截器的操纵以使得移动目标被拦截。

105. 发明申请

US20120053764A1 PARTICLE SWARM-BASED MICRO AIR LAUNCH VEHICLE TRAJECTORY OPTIMIZATION METHOD 有权
标题翻译：基于微波的微型飞行器车辆轨道优化方法
公开(公告)号：US20120053764A1
公开(公告)日：2012-03-01
申请号：US12871649
申请日：2010-08-30
申请人： HANAFY M. OMAR , MOUMEN M. IDRES , RAED KAFAFY
发明人： HANAFY M. OMAR , MOUMEN M. IDRES , RAED KAFAFY
IPC分类号： G05D1/00
CPC分类号： G05D1/107
摘要： The particle swarm-based micro air launch vehicle trajectory optimization method is carried out by formulating a parameter optimization problem, which is solved using a particle swarm optimization procedure. The optimization problem is formulated using a single objective function having the explicit objective to maximize the payload mass. Constraints on terminal conditions are imposed.
摘要翻译：基于粒子群的微型空中发射车轨迹优化方法是通过制定一个参数优化问题进行的，该问题是使用粒子群优化程序解决的。使用具有明确目标的单个目标函数来形成优化问题，以使有效负载质量最大化。限制终端条件的限制。

106. 发明授权

US07298255B1 Sensory systems employing non-uniformly spaced waveguide sensors for determining orientation and rotational speed of objects 有权
标题翻译：感应系统采用不均匀间隔的波导传感器来确定物体的方位和转速
公开(公告)号：US07298255B1
公开(公告)日：2007-11-20
申请号：US11161413
申请日：2005-08-02
申请人： Carlos M. Pereira , Hai-Long Nguyen
发明人： Carlos M. Pereira , Hai-Long Nguyen
IPC分类号： H04Q1/08 , G01S13/58
CPC分类号： G01S1/14 , F41G7/346 , F41G7/36 , G01S1/16 , G01S3/146 , G01S3/30 , G05D1/107
摘要： A sensory system for determining the orientation of an object, wherein the sensory system includes a plurality of non-uniformly spaced waveguide sensors or array(s) of waveguide sensors. The non-uniformly spaced waveguide sensors are responsive to received radio frequency signals wherein the received power of the signals is dependent upon the orientation of the waveguide(s).
摘要翻译：用于确定物体的取向的感觉系统，其中所述感觉系统包括多个不均匀间隔的波导传感器或波导传感器的阵列。不均匀间隔的波导传感器响应于接收的射频信号，其中信号的接收功率取决于波导的取向。

107. 发明授权

US07137208B2 Leveling device 失效
标题翻译：调平装置
公开(公告)号：US07137208B2
公开(公告)日：2006-11-21
申请号：US10905077
申请日：2004-12-14
申请人： Ray F. Campbell , Joan D. Wada
发明人： Ray F. Campbell , Joan D. Wada
IPC分类号： G01P15/00 , G01C9/06
CPC分类号： G05D1/107 , F42B15/01 , G01C9/00 , G01P15/125 , G01P15/18
摘要： A leveling system for a missile system includes a holder defining an xz-plane. Four flexure plate accelerometers are coupled to the holder at angles such that they are sensitive to movement in an xy-plane. The accelerometers all generate signals in response to movements of the flexure plates. An actuator activates an object control device in response to a platform control signal. A processor receives the accelerometer signals and generates the platform control signal in response thereto.
摘要翻译：用于导弹系统的调平系统包括限定xz平面的支架。四个挠曲板加速度计以与XY平面中的运动敏感的角度联接到保持器。加速度计全部响应挠曲板的移动而产生信号。执行器响应于平台控制信号激活对象控制装置。处理器接收加速度计信号并响应于此产生平台控制信号。

108. 发明授权

US06785610B2 Spatial avoidance method and apparatus 有权
标题翻译：空间回避方法和装置
公开(公告)号：US06785610B2
公开(公告)日：2004-08-31
申请号：US10168700
申请日：2002-06-20
申请人： Brian C. Baker , Scott J. Paynter
发明人： Brian C. Baker , Scott J. Paynter
IPC分类号： G06F1550
CPC分类号： G05D1/104 , G05D1/107
摘要： An obstacle avoidance system, apparatus, and method is described suitable for use on autonomously guided or man-in-the-loop guided vehicles such as aircraft, missiles, cars, and other types of vehicles. The system provides guidance instructions in the situation where the vehicle encounters an obstacle either directly or indirectly in its path while traveling to a desired destination or where vehicles are traveling in formation. The system can be applied not only to obstacle avoidance but also to trajectory shaping by defining obstacles, operational boundaries and/or threats which influence the trajectory of the vehicle.
摘要翻译：描述了适用于自主引导或人在环路导向的车辆如飞机，导弹，汽车和其他类型的车辆的障碍物回避系统，装置和方法。该系统在车辆在行进到期望的目的地或者车辆行进在地面中时直接或间接地在其路径中遇到障碍物的情况下提供指导说明。该系统不仅可以应用于障碍物回避，而且可以通过定义影响车辆轨迹的障碍物，操作边界和/或威胁来应用轨迹成形。

109. 发明授权

US06695251B2 Method and system for synchronized forward and Aft thrust vector control 有权
标题翻译：同步向前和向后推力矢量控制的方法和系统
公开(公告)号：US06695251B2
公开(公告)日：2004-02-24
申请号：US09883622
申请日：2001-06-19
申请人： John J. Rodden , Andrew E. Turner
发明人： John J. Rodden , Andrew E. Turner
IPC分类号： F42B1002
CPC分类号： G05D1/107
摘要： A system for controlling attitude about pitch, yaw, and roll axes and axial thrust of a body. The system comprises a main thrust generator located on an aft portion of the body and at least one reaction control system (RCS) located on a forward portion of the body. A thrust vector controller (TVC) is connectable to the main thrust generator and at least one RCS controller is connectable to the RCS. The RCS controller and the TVC are synchronized to adjust the direction of the principal line of thrust through the body center of gravity.
摘要翻译：用于控制身体的俯仰，偏转和滚动轴线的轴向推力的姿态的系统。该系统包括位于身体的后部的主推力发生器和位于身体前部的至少一个反应控制系统（RCS）。推力矢量控制器（TVC）可连接到主推力发生器，并且至少一个RCS控制器可连接到RCS。 RCS控制器和TVC被同步，以调整通过人体重心的推力主线的方向。

110. 发明授权

US06629668B1 Jump correcting projectile system 失效
标题翻译：跳弹校正系统
公开(公告)号：US06629668B1
公开(公告)日：2003-10-07
申请号：US10062092
申请日：2002-02-04
申请人： John C. Grau , Arthur J. Fiorellini , Raymond E. Carr
发明人： John C. Grau , Arthur J. Fiorellini , Raymond E. Carr
IPC分类号： F42B1000
CPC分类号： G05D1/107 , F41G7/22 , F42B10/661
摘要： A system for controlling the trajectory of a launched projectile. More particularly, a method for correcting the projectile jump displacement of a launched projectile after it is released from a vessel using on-board G-hardened accelerometers orthogonally mounted along the longitudinal axis of the projectile. Deviation from an intended flight path is corrected by firing selected trajectory diverting thrusters mounted around the periphery of the projectile. Eliminating or reducing projectile jump, or the angular deviation of the flight path of a projectile relative to its intended trajectory, will greatly increase the accuracy of gun fired projectiles.
摘要翻译：一种用于控制发射射弹轨迹的系统。更具体地说，一种用于校正所发射的抛射体在使用沿着射弹的纵向轴线正交安装的车载G硬化加速度计从船舶释放之后的弹丸跳跃位移的方法。通过点燃安装在射弹周边的选定的轨道转向推进器来校正与预期飞行路径的偏差。消除或减少射弹跳跃或射弹的飞行路径相对于其预期轨迹的角度偏差将大大提高炮弹射弹的精度。

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