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91. 发明申请

US20070255524A1 System and method for computing reachable areas 失效
标题翻译：用于计算可到达区域的系统和方法
公开(公告)号：US20070255524A1
公开(公告)日：2007-11-01
申请号：US11413925
申请日：2006-04-27
申请人： Peter Tinker , David Payton
发明人： Peter Tinker , David Payton
IPC分类号： G01C17/00
CPC分类号： F41G7/007 , F41G9/00
摘要： The present invention relates to computing reachable areas given a first point. More specifically, the present invention relates to the computation of an intersection between a first surface and a second surface for determining a set of points that are reachable from a first point. Using the present invention, a user can determine either (1) a locus of target sites that can be struck by a ballistic projectile from a given launch site, or (2) a locus of launch sites that can be used to hit a given target site. The disclosed system and method employs graphics hardware to determine an intersection between a first surface defined by trajectory paths, and a second surface defined by terrain.
摘要翻译：本发明涉及计算可达到的第一点的区域。更具体地，本发明涉及第一表面和第二表面之间的交叉点的计算，用于确定从第一点可到达的一组点。使用本发明，用户可以确定（1）可以从给定发射场点被弹道射弹击中的目标位置的轨迹，或者（2）可用于击中给定目标的发射场所的轨迹现场。所公开的系统和方法使用图形硬件来确定由轨迹路径限定的第一表面和由地形限定的第二表面之间的交点。

92. 发明申请

US20070244673A1 METHODS AND APPARATUS FOR OPTIMAL RESOURCE ALLOCATION 有权
标题翻译：最优资源分配的方法和装置
公开(公告)号：US20070244673A1
公开(公告)日：2007-10-18
申请号：US11279824
申请日：2006-04-14
申请人： Deepak Khosla , Thomas Nichols
发明人： Deepak Khosla , Thomas Nichols
IPC分类号： F41F5/00 , G06F17/10
CPC分类号： F41G3/04 , F41G7/007 , G06Q10/06 , G06Q10/067
摘要： Method and apparatus to automatically allocate and schedule weapon systems to threats for maximizing an engagement objective. In one aspect, methods and systems maximize threat killed. In another aspect, methods and systems maximize asset survival against threats. The methods and apparatus considers temporal and resource constraints such that weapons systems are able to engage threats assigned to them.
摘要翻译：自动分配和安排武器系统的威胁的方法和装置，以最大化接合目标。在一个方面，方法和系统最大限度地杀死了威胁。另一方面，方法和系统可以最大限度地利用威胁来实现资产生存。方法和设备考虑到时间和资源的限制，使得武器系统能够参与分配给他们的威胁。

93. 发明授权

US07083139B2 Method for guiding a rocket 失效
标题翻译：引导火箭的方法
公开(公告)号：US07083139B2
公开(公告)日：2006-08-01
申请号：US10490951
申请日：2002-09-23
申请人： Michel Broekaert
发明人： Michel Broekaert
IPC分类号： F41G7/00
CPC分类号： F41G7/2293 , F41G7/007 , F41G7/2206 , F41G7/2253
摘要： Method for guiding a rocket (1) to a target, wherein, the rocket (1) being equipped with automatic guiding means with an image-formation device (10) and means for correction of the trajectory (11): the target is acquired by a sighting device and its position is determined; the sighting device and the rocket image-formation device (10) are brought into line; the images of the rocket image-formation device (10) are stabilized; a guiding law is produced; the rocket (1) is launched; and the rocket is guided according to this law until the rocket itself acquires the target.
摘要翻译：用于将火箭（1）引导到目标的方法，其中，配备有具有图像形成装置（10）的自动引导装置的火箭（1）和用于校正轨迹（11）的装置：目标是通过瞄准装置及其位置确定; 瞄准装置和火箭图像形成装置（10）被并入; 火箭图像形成装置（10）的图像稳定; 制定了指导性法律; 火箭（1）发射; 火箭依照本法规定，直到火箭本身获得目标。

94. 发明申请

US20050234605A1 Alignment of a flight vehicle based on recursive matrix inversion 有权
标题翻译：基于递归矩阵求逆的飞行器对准
公开(公告)号：US20050234605A1
公开(公告)日：2005-10-20
申请号：US10827229
申请日：2004-04-19
申请人： Shing Kau
发明人： Shing Kau
IPC分类号： F41G3/32 , F41G7/00 , G01C21/16 , B64C1/00
CPC分类号： F41G3/326 , F41G7/007
摘要： A method for recursively determining alignment of a flight vehicle during flight is provided. The method includes generating data in a reference coordinate frame and in a second coordinate frame at a plurality of points in time during the flight, recursively generating first and second matrices from the data in the reference coordinate frame and the second coordinate frame, and at each point in time, determining an alignment output based on the inverted first matrix and the second matrix.
摘要翻译：提供了一种用于在飞行中递归地确定飞行器的对准的方法。该方法包括在飞行期间在多个时间点的参考坐标系和第二坐标系中生成数据，并从每个基准坐标系和第二坐标系中的数据递归地生成第一和第二矩阵基于反转的第一矩阵和第二矩阵来确定对准输出。

95. 发明申请

US20050223883A1 Standoff land attack-expanded response device computer 审中-公开
标题翻译：间谍土地攻击扩展响应设备计算机
公开(公告)号：US20050223883A1
公开(公告)日：2005-10-13
申请号：US10796218
申请日：2004-03-09
申请人： Aaron Eggemeyer , James Leonard , Robert Menzel , Richard Meyer
发明人： Aaron Eggemeyer , James Leonard , Robert Menzel , Richard Meyer
IPC分类号： B64D1/04 , B64D7/00 , H04L29/08
CPC分类号： B64D7/00 , F41G7/007 , H04L67/12
摘要： A system for an aircraft that includes an attachment point for a store and a data management system that communicates data amongst a plurality of mobile platform systems and an operator. The data management system includes a docking station and a data link operatively associated with the attachment point thereby allowing the store and at least one of the mobile platform systems to communicate. The system includes a circuit that docks to the docking station and includes an input, a first data port, and a second data port. The circuit accepts operator commands via the input and sends commands to the data link, and to the store, based on the inputs via the second data port. Additionally, the circuit accepts imaging from the store via the second data port.
摘要翻译：一种用于飞机的系统，其包括用于商店的附接点和在多个移动平台系统和操作者之间传送数据的数据管理系统。数据管理系统包括对接站和与附接点可操作地相关联的数据链路，从而允许存储和至少一个移动平台系统进行通信。该系统包括一个与对接站对接并包括输入端，第一数据端口和第二数据端口的电路。该电路通过输入接受操作员命令，并通过第二个数据端口根据输入向数据链路和存储发送命令。此外，电路经由第二数据端口接收来自商店的成像。

96. 发明申请

US20050183570A1 SELF-CONTAINED AIRBORNE SMART WEAPON UMBILICAL CONTROL CABLE 有权
标题翻译：自包含AIRBORNE智能武器脐带电缆
公开(公告)号：US20050183570A1
公开(公告)日：2005-08-25
申请号：US10754153
申请日：2004-01-09
申请人： Roy McMahon
发明人： Roy McMahon
IPC分类号： F41G7/00 , F42C15/40 , F42C17/04 , F41F5/00
CPC分类号： F42C15/40 , F41G7/001 , F41G7/007 , F42C17/04
摘要： An umbilical cable for delivering electrical signals between an aircraft and a smart weapon carried by the aircraft. The umbilical cable includes cabling comprising a plurality of conductive wires, a first connector provided on one end of the cabling and configured to connect to the aircraft, and a second connector provided on the other end of the cabling and configured to connect to the smart weapon. The umbilical cable further includes an interface circuit electrically coupled between the first connector and the second connector via the plurality of conductive wires. The interface circuit is configured to receive via the first connector a non-standard combination of signals comprising at least one of data signals, control signals and power signals not receivable directly by the smart weapon to carry out operations. Moreover, the interface circuit is configured to convert the non-standard combination of signals to a set of signals receivable by the smart weapon to carry out operations, and to provide the set of receivable signals to the smart weapon via the second connector.
摘要翻译：用于在飞行器和飞机携带的智能武器之间传递电信号的脐带缆。脐带缆包括布线，其包括多根导线，设置在布线的一端并被配置为连接到飞行器的第一连接器，以及设置在电缆的另一端并被配置成连接到智能武器的第二连接器。脐带缆还包括经由多根导线电连接在第一连接器和第二连接器之间的接口电路。接口电路被配置为经由第一连接器接收包括数据信号，控制信号和智能武器直接不能接收的功率信号中的至少一个的非标准组合，以执行操作。此外，接口电路被配置为将信号的非标准组合转换成由智能武器可接收的一组信号，以执行操作，并且经由第二连接器向智能武器提供可接收信号的集合。

97. 发明申请

US20050031125A1 Global-positioning-system data integrator and distribution system 审中-公开
标题翻译：全球定位系统数据集成商和分销系统
公开(公告)号：US20050031125A1
公开(公告)日：2005-02-10
申请号：US10881786
申请日：2004-06-30
申请人： Arthur Acampora , Donald Anderson , Richard Anthony
发明人： Arthur Acampora , Donald Anderson , Richard Anthony
IPC分类号： G01S19/48 , F41G7/00 , F41G7/30 , G01S19/09 , G01S19/39 , G08G5/00 , H04K1/00 , H04L9/08
CPC分类号： F41G7/007 , G01S19/03 , G01S19/05
摘要： A weapons system is disclosed that provides hot-start navigational information to the Global-Positioning-System receivers on missiles prior to flight. The system comprises a Global-Positioning-System receiver that uses a classified red cryptographic key to decode the P(Y) signal from one or more of the Global-Positioning-System constellation of satellites. Once the P(Y) signal is decoded, one or more characteristics (e.g., the PRN code synchronization, the Doppler shift, the modulation bit sequence, etc.) of the signal is derived. These characteristics of the signal—and some other information including a black cryptographic key that comprises the red cryptographic key—are then provided to the Global-Positioning-System receivers on missiles prior to flight. By giving the missiles this information, the missiles are able to acquire the P(Y) signals themselves more quickly than they otherwise could, which enables them to determine their position more quickly than they otherwise could.
摘要翻译：公开了一种武器系统，其在飞行前向导弹的全球定位系统接收机提供热启动导航信息。该系统包括全球定位系统接收机，其使用分类的红色加密密钥来解码来自卫星的全球定位系统星座中的一个或多个的P（Y）信号。一旦解码了P（Y）信号，就得出信号的一个或多个特性（例如，PRN码同步，多普勒频移，调制比特序列等）。然后，信号的这些特征以及包括红色加密密钥的黑色加密密钥的一些其他信息在飞行前在导弹上提供给全球定位系统接收机。通过给导弹这个信息，导弹能够比其他方式更快地获取P（Y）信号，这使得他们能够比其他方式更快地确定它们的位置。

98. 发明授权

US06491253B1 Missile system and method for performing automatic fire control 失效
标题翻译：导弹系统和执行自动火灾控制的方法
公开(公告)号：US06491253B1
公开(公告)日：2002-12-10
申请号：US06754890
申请日：1985-04-15
申请人： Pat H. McIngvale
发明人： Pat H. McIngvale
IPC分类号： F41G700
CPC分类号： F41G7/2226 , F41G3/02 , F41G7/007 , F41G7/2206 , F41G7/2253 , F41G7/2293
摘要： A missile system and method for performing automatic fire control in which a reconnaissance vehicle is used to gather video reference information of a target and this information is then communicated to a launching vehicle from which missiles are caused to be trained on the selected target by utilizing an automatic target handoff correlator that identifies the selected target, causes an autotracker to be locked on and finally a computer is signaled by the automatic target handoff correlator to cause a missile to be fired.
摘要翻译：一种用于进行自动消防控制的导弹系统和方法，其中使用侦察车辆来收集目标的视频参考信息，并且该信息然后被传送到发射车辆，导弹通过利用导弹将导弹训练在所选择的目标上自动目标切换相关器，其识别所选择的目标，导致自动跟踪器被锁定，并且最终由自动目标切换相关器发信号通知计算机以导致导弹被触发。

99. 发明授权

US06122569A Store interface apparatus 有权
标题翻译：存储接口设备
公开(公告)号：US06122569A
公开(公告)日：2000-09-19
申请号：US191884
申请日：1998-11-13
申请人： William J. Ebert , James V. Leonard , Richard E. Meyer
发明人： William J. Ebert , James V. Leonard , Richard E. Meyer
IPC分类号： F41G7/00 , G06F7/00
CPC分类号： F41G7/007
摘要： A store interface for routing different types of store signal formats to multiple wing stations using pre-existing aircraft wing wiring. The store interface provides an interface between an aircraft and an associated store adapted to bidirectionally communicate with the aircraft according to one of a plurality of predetermined store signal formats. The store interface includes a store identifier that determines the type of the associated store, and an interface that bidirectionally communicates between the aircraft and the store, includinga first and second communication links that communicate with the store using either a first set of store control signals configured in accordance with a first store signal format or a second set of store control signals configured in accordance with a second store signal format. The store interface also includes a switch that couples one of the communication links to the store in response to the store identifier allowing one of the sets of store control signals to be transmitted between the aircraft and the store.
摘要翻译：存储接口，用于使用预先存在的飞机机翼布线将不同类型的存储信号格式路由到多个机位站。存储界面提供了根据多个预定存储信号格式之一的适于与飞机双向通信的飞行器和相关联存储器之间的接口。存储界面包括确定相关存储的类型的商店标识符以及在飞机和商店之间双向通信的接口，包括使用第一组存储控制信号与商店通信的第一和第二通信链路根据第一存储信号格式或根据第二存储信号格式配置的第二组存储控制信号配置。存储接口还包括响应于存储标识符将通信链路之一耦合到存储器的开关，允许在飞机和商店之间传输存储控制信号组中的一个。

100. 发明授权

US6057949A Bi-directional infrared communications system 失效
标题翻译：双向红外通信系统
公开(公告)号：US6057949A
公开(公告)日：2000-05-02
申请号：US908275
申请日：1997-08-07
申请人： Gary A. Kinstler
发明人： Gary A. Kinstler
IPC分类号： F41G7/00 , H04B10/00
CPC分类号： F41G7/007
摘要： An infrared (IR) transmitter modulator/receiver controller (TM/RC) encodes downlink serial digital data and precise time synchronization strobes from a host system to provide a downlink modulated serial digital electrical waveform. At least one IR host system transceiver (HST) converts the downlink modulated serial digital electrical waveform to a modulated downlink IR light waveform. At least one IR remote device transceiver (RDT) receives the modulated downlink IR light waveform from the HST. Each RDT is connected to a remote device. The modulated downlink IR light waveform is converted into a corresponding electrical waveform and further demultiplexed into its downlink serial digital data and precise time synchronization strobes. Each RDT provides an uplink electrical and IR modulated serial digital waveform to be received by the HST for conversion to an uplink demodulated serial digital electrical waveform. The HST transfers the uplink demodulated serial digital electrical waveforms to the TM/RC, thus providing a multiplexed combination of data and time information on the downlink and communication of uplink status information from the remote devices.
摘要翻译：红外（IR）发射机调制器/接收机控制器（TM / RC）编码来自主机系统的下行链路串行数字数据和精确的时间同步选通以提供下行链路调制的串行数字电波形。至少一个IR主机系统收发器（HST）将下行链路调制的串行数字电波形转换成调制的下行链路IR光波形。至少一个IR远程设备收发器（RDT）从HST接收调制的下行链路IR光波形。每个RDT连接到远程设备。调制的下行链路IR光波形被转换成相应的电波形，并进一步解复用为其下行链路串行数字数据和精确的时间同步脉冲。每个RDT提供由HST接收的用于转换为上行链路解调的串行数字电波形的上行链路电和IR调制串行数字波形。 HST将上行解调的串行数字电波形传送到TM / RC，从而提供下行链路上的数据和时间信息的复用组合以及来自远程设备的上行链路状态信息的通信。

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