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1. 发明授权

US4949089A Portable target locator system 失效
标题翻译：便携式目标定位系统
公开(公告)号：US4949089A
公开(公告)日：1990-08-14
申请号：US398188
申请日：1989-08-24
申请人： Robert A. Ruszkowski, Jr.
发明人： Robert A. Ruszkowski, Jr.
IPC分类号： G01S5/14 , G01S7/00 , G01S13/86 , G01S19/51
CPC分类号： F41G3/02 , F41G3/06 , G01S17/023 , G01S7/003
摘要： A portable target locator system capable of being transported and utilized by an individual combatant is disclosed. The portable target locator system comprises a rifle-like target locator and a transmitter/modem capable of transmitting target location coordinates to a weapons delivery system. The rifle-target locator preferably includes a Global Positioning System (GPS) receiver capable of determining the location coordinates of the target locator automatically and with a high degree of accuracy from signals transmitted from a network of orbiting satellites. A laser rangefinder and digital azimuth and inclination sensor are then utilized to accurately determine the range, azimuth and inclination of an identified target from the target locator. This information is then processed in conjunction with the location coordinates of the target locator to generate location coordinates for the selected target. The target location coordinates are then coupled to the transmitter/modem for transmittal to a remotely located control system, such as a weapons delivery system. In one preferred embodiment of the present invention a non-volatile memory is provided and multiple target coordinate sets are then stored within the memory and subsequently transmitted to the weapons delivery system during a single transmission.
摘要翻译：公开了能够由个人战斗员运输和利用的便携式目标定位系统。便携式目标定位器系统包括步枪式目标定位器和能够将目标位置坐标传送到武器传送系统的发射机/调制解调器。步枪目标定位器优选地包括全球定位系统（GPS）接收机，能够自动地以高精确度地从轨道卫星网络发送的信号来确定目标定位器的位置坐标。然后使用激光测距仪和数字方位角和倾角传感器来精确地确定来自目标定位器的识别目标的范围，方位角和倾斜度。然后结合目标定位器的位置坐标来处理该信息，以生成所选目标的位置坐标。然后将目标位置坐标耦合到发射机/调制解调器，以传送到远程位置的控制系统，例如武器传送系统。在本发明的一个优选实施例中，提供非易失性存储器，然后将多个目标坐标组存储在存储器内，随后在单个传输期间传送到武器传送系统。

2. 发明授权

US06674391B2 System and method of simulated image reconstruction 失效
标题翻译：模拟图像重建的系统和方法
公开(公告)号：US06674391B2
公开(公告)日：2004-01-06
申请号：US10141321
申请日：2002-05-08
申请人： Robert A. Ruszkowski, Jr.
发明人： Robert A. Ruszkowski, Jr.
IPC分类号： G01S1390
CPC分类号： H04N19/507 , H04N19/593
摘要： A system includes a storage medium storing contextual information about a target or target area, and a simulator communicatively coupled to the storage medium and operable to receive the contextual information. The simulator is operable to generate a set of simulated information about the target using the contextual information. The system further includes a sensor operable to collect a set of actual information about the target. A comparator is operable to generate a set of delta information in response to differences between the set of simulated information and the set of actual information. The delta information is transmitted and added to a second set of simulated information to generate a set of information that is substantially similar to the set of actual information.
摘要翻译：一种系统包括存储关于目标区域或目标区域的上下文信息的存储介质，以及通信地耦合到存储介质并可操作以接收上下文信息的模拟器。模拟器可操作以使用上下文信息生成关于目标的一组模拟信息。该系统还包括可操作以收集关于目标的一组实际信息的传感器。比较器可操作以响应于所述一组模拟信息与所述一组实际信息之间的差异来生成一组增量信息。增量增量信息被发送并添加到第二组模拟信息中以生成基本上类似于实际信息集合的一组信息。

3. 发明授权

US07097136B2 Immersible unmanned air vehicle and system for launch, recovery, and re-launch at sea 失效
标题翻译：潜艇无人机和发射，恢复和重新发射的系统
公开(公告)号：US07097136B2
公开(公告)日：2006-08-29
申请号：US10823434
申请日：2004-04-13
申请人： Robert A. Ruszkowski, Jr.
发明人： Robert A. Ruszkowski, Jr.
IPC分类号： B64C35/00
CPC分类号： B64C1/062 , B63G8/28 , B63G8/30 , B63G13/00 , B64C35/00 , B64C37/00 , B64C39/024 , B64C2001/0045 , B64C2201/048 , B64C2201/084 , B64C2201/121 , B64C2201/127 , B64C2201/141 , B64C2201/205 , F41F3/07 , F42B15/20
摘要： A sea-launched and recovered unmanned aircraft is disclosed. The aircraft is jet-powered and has features and systems to maintain watertight integrity such that it may be released from a submerged submarine or dropped into a body of water by a ship or an aircraft. The aircraft is buoyant and remains at or near the water surface before its rockets are ignited. The rockets propel the air vehicle out of the sea and accelerate it to flying speed at which time a jet engine is started and the rockets are jettisoned. The air vehicle performs its mission independently or in conjunction with other ones of the air vehicles. The air vehicle then returns to an assigned splashdown point at sea via, for example, an engine-off “whip-stall” maneuver. A submarine or ship may retrieve the air vehicle and readies it for another mission.
摘要翻译：披露了一架海上发射和回收的无人机。飞机是喷气式动力的，并具有保持水密完整性的特征和系统，使得其可以从潜水艇释放或由船或飞机落入水体。这架飞机是浮力的，并且在其火箭点火之前保持在水面或附近。火箭将空中车辆推出海面，并将其加速到飞行速度，此时起飞喷气发动机，火箭被抛弃。机动车辆独立地或与其他机动车辆一起执行任务。然后，空中飞行器通过例如发动机关闭“鞭炮”操纵返回到海上指定的飞溅点。潜艇或船只可以检索空中飞行器并准备进行另一个飞行任务。

4. 发明授权

US5717397A Low observable shape conversion for aircraft weaponry 失效
标题翻译：飞机武器的低可观测形状转换
公开(公告)号：US5717397A
公开(公告)日：1998-02-10
申请号：US649213
申请日：1996-05-17
申请人： Robert A. Ruszkowski, Jr.
发明人： Robert A. Ruszkowski, Jr.
IPC分类号： B64D7/00 , F41H3/00 , F42B25/00 , H01Q17/00
CPC分类号： B64D7/00 , F41H3/00 , F42B25/00 , H01Q17/00
摘要： An apparatus for encapsulating a warhead or bomb for the purpose of reducing the weapon's radar cross-section, including a hollow jacket and a hollow tail section. The warhead is inserted into the specially-shaped jacket and into at least part of the tail section. The jacket is secured to the warhead by lugs and the tail section is secured to the jacket or to the warhead. The jacket has two pointed seams on opposite sides of a vertical plane passing through the warhead pointing outward from the vertical plane and which extend along the length of the jacket. The front of the tail section has a serrated edge which overlaps the rear end of the jacket. The tail section has horizontal fins and downward and outward extending fins. The lugs allow the apparatus to be releaseably attached to the bottom the fuselage or the bottom of a wing pylon of a military aircraft.
摘要翻译：用于封装弹头或炸弹的装置，用于减少武器的雷达横截面，包括中空护套和中空尾部。将弹头插入特殊外套并进入尾部的至少部分。护套通过凸耳固定在弹头上，尾部固定在护套或弹头上。护套在垂直平面的相对侧上具有两条尖锐的接缝，该垂直平面穿过从垂直平面向外指向的弹头，并且沿着护套的长度延伸。尾部的前部具有与夹克的后端重叠的锯齿状边缘。尾部具有水平翅片，向下和向外延伸的翅片。凸耳允许设备可释放地附接到机身的底部或军用飞机的机翼塔的底部。

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