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    • 1. 发明授权
    • Apparatus and method for locating an emitter using RF carrier or PRF
measurement ratios
    • 使用RF载波或PRF测量比定位发射器的装置和方法
    • US06163297A
    • 2000-12-19
    • US421286
    • 1999-10-20
    • Conrad M. Rose
    • Conrad M. Rose
    • G01S3/52G01S5/04G01S7/02
    • G01S5/04G01S3/52G01S7/021
    • A method and apparatus for determining from a moving observer the location, in terms of latitude, longitude, altitude, and velocity, of a stationary or moving radar emitting a pulsed or continuous-wave signal. The moving observer extracts from the radar signal significant electronic support measures (ESM) parameters, including frequency, pulse repetition interval, and pulse width, and determines from those parameters whether a radio frequency (RF) or pulse repetition frequency (PRF) measurement technique is appropriate, and whether the radar signal angle-of-arrival (AOA) must be computed. The emitter location is computed using a ratio of sequential frequency measurements, and the moving observer continues to collect frequency measurements until the location of the emitter can be established to within a predetermined degree of certainty.
    • 一种用于从移动观测器确定发射脉冲或连续波信号的静止或运动雷达的纬度,经度,高度和速度的方式和装置。 移动观测器从雷达信号中提取重要的电子支持措施(ESM)参数,包括频率,脉冲重复间隔和脉冲宽度,并根据这些参数确定射频(RF)或脉冲重复频率(PRF)测量技术是否为 是否必须计算雷达信号到达角(AOA)。 使用顺序频率测量的比率来计算发射器位置,并且移动观察者继续收集频率测量,直到发射器的位置可以被建立到预定的确定度之内。
    • 2. 发明授权
    • Emitter location using RF carrier or PRF measurement ratios
    • 使用RF载波或PRF测量比的发射器位置
    • US6100845A
    • 2000-08-08
    • US996507
    • 1997-12-23
    • Conrad M. Rose
    • Conrad M. Rose
    • G01S3/52G01S5/04G01S7/02G01S5/02G01S13/00
    • G01S5/04G01S3/52G01S7/021
    • A method and apparatus for determining from a moving observer the location, in terms of latitude, longitude, altitude, and velocity, of a stationary or moving radar emitting a pulsed or continuous-wave signal. The moving observer extracts from the radar signal significant electronic support measures (ESM) parameters, including frequency, pulse repetition interval, and pulse width, and determines from those parameters whether a radio frequency (RF) or pulse repetition frequency (PRF) measurement technique is appropriate, and whether the radar signal angle-of-arrival (AOA) must be computed. The emitter location is computed using a ratio of sequential frequency measurements, and the moving observer continues to collect frequency measurements until the location of the emitter can be established to within a predetermined degree of certainty.
    • 一种用于从移动观测器确定发射脉冲或连续波信号的静止或运动雷达的纬度,经度,高度和速度的方式和装置。 移动观测器从雷达信号中提取重要的电子支持措施(ESM)参数,包括频率,脉冲重复间隔和脉冲宽度,并根据这些参数确定射频(RF)或脉冲重复频率(PRF)测量技术是否为 是否必须计算雷达信号到达角(AOA)。 使用顺序频率测量的比率来计算发射器位置,并且移动观察者继续收集频率测量,直到发射器的位置可以被建立到预定的确定度之内。
    • 3. 发明授权
    • Method of detection and determining an angular location of frequency agile emitters
    • 检测和确定频率敏捷发射器角位置的方法
    • US06313794B1
    • 2001-11-06
    • US09487209
    • 2000-01-19
    • Conrad M. Rose
    • Conrad M. Rose
    • G01S502
    • G01S3/48
    • The present invention uses feedback 300 from RF carrier frequency measurements 301 to disassociate the emitter angle-of-arrival component 313 in the ambiguous phase measurement 312 from the initially unknown phase measurement integer ambiguities 314; to then process 302 resolve the ambiguities; and finally to process 303 to obtain the correct emitter AOA. The present invention does this by converting the actual interferometer baselines 315 on which the unassociated pulse 308 phase measurements 304 were made at different emitter frequencies to a baseline set 305 for a single-frequency equivalent interferometer array. This conceptual array has the following property: the phase measurement 306 that would be made on it at the fixed frequency for a signal at the same direction-of-arrival 307 are identical to the actual phase measurements made on the physical array. Because of this equivalency the conceptual array is called the E(equivalent)-array. But, whereas the physical array has antenna spacings 317 that are invariant, the E-array “antenna” spacings 316 change as a function of the RF carrier frequency measurement feedback 300, which depends on the particular residual pulses being tested. Thus there is a different E-array, even for the same frequency agile emitter, depending on the particular residual pulse set 309 used.
    • 本发明使用来自RF载波频率测量301的反馈300将模糊相位测量312中的发射器到达分量313与最初未知的相位测量整数模糊度314分离; 然后处理302解决歧义; 最后进行处理303以获得正确的发射器AOA。 本发明通过将不相关的脉冲30​​8相位测量304的不相关脉冲308相位测量304的实际干涉仪基线315转换成单频等效干涉仪阵列的基线组305来实现。 该概念阵列具有以下属性:将以相同的到达方向307处的信号以固定频率在其上进行的相位测量306与在物理阵列上进行的实际相位测量相同。 由于这个等价性,概念数组被称为E(等价) - 数组。 但是,尽管物理阵列具有不变的天线间隔317,但是E阵列“天线”间隔316作为RF载波频率测量反馈300的函数而变化,这取决于被测试的特定残留脉冲。 因此,即使对于相同频率的敏捷发射器也存在不同的E阵列,这取决于所使用的特定残留脉冲集309。
    • 4. 发明授权
    • Multiplatform ambiguous phase circle and TDOA protection emitter location
    • 多平面模糊相位和TDOA保护发射极位置
    • US5999129A
    • 1999-12-07
    • US88196
    • 1998-06-01
    • Conrad M. Rose
    • Conrad M. Rose
    • G01S5/12G01S1/30G01S1/24
    • G01S5/12
    • A method and system for determining the geolocation--i.e., the latitude, longitude, and altitude--of a stationary RF signal emitter from two or more moving observer aircraft. The observers receive signals from the emitter and the system measures the phase difference between the signals. The observers then perform pulse time of arrival (TOA) measurements over a predetermined clock interval, and calculate the time difference of arrival (TDOA) of corresponding, same-pulse, emitter signals. Based on geometric relationships, the system creates a series of circular lines of position (LOPs) for each observer, and computes hyperbolic LOPs based on the TDOA calculations. The system determines emitter location from the intersection of the hyperbolic LOPs and the circular LOPs.
    • 用于确定来自两个或更多个移动观察员飞机的固定RF信号发射器的地理位置的方法和系统,即纬度,经度和高度。 观察者从发射器接收信号,并且系统测量信号之间的相位差。 观察者然后在预定的时钟间隔内执行到达时间(TOA)测量,并且计算相应同脉冲发射器信号的到达时间差(TDOA)。 基于几何关系,系统为每个观察者创建一系列圆形位置(LOP),并根据TDOA计算计算双曲线LOP。 该系统从双曲线LOP和圆形LOP的交点确定发射器位置。
    • 6. 发明授权
    • Emitter frequency-time measurement by a moving observer using no
navigation input
    • 使用无导航输入的移动观察者进行发射器频率测量
    • US5534866A
    • 1996-07-09
    • US499825
    • 1995-07-10
    • Conrad M. Rose
    • Conrad M. Rose
    • G01S7/02G01S7/36G01S7/40G01S7/285
    • G01S7/021G01S7/36
    • A method for determining a constant classification parameter for a radar is described; this parameter uniquely characterizes and identifies the radar being monitored. The method does not require the use of navigation or orientation information concerning the observer platform. The emitter pulse repetition frequency (PRF) provides a clock signal to allow measurement of the number of cycles of emitter carrier occurring in a predetermined interval. This value is the same at the emitter and at the observer and forms the aforementioned classification parameter. The classification parameter is additionally used to detect the presence of countermeasures designed to defeat passive Doppler emitter location.
    • 描述了用于确定雷达的常数分类参数的方法; 该参数独特地表征并识别被监测的雷达。 该方法不需要使用关于观察者平台的导航或方向信息。 发射极脉冲重复频率(PRF)提供时钟信号,以允许以预定的间隔测量发射器载体的周期数。 该值在发射器和观察者处相同并形成上述分类参数。 分类参数还用于检测设计用于消除被动多普勒发射器位置的对策的存在。
    • 7. 发明授权
    • (AOA/LBI) emitter ranging method and apparatus
    • (AOA / LBI)发射器测距方法和装置
    • US5343212A
    • 1994-08-30
    • US992965
    • 1992-12-11
    • Conrad M. RoseJeffrey J. Drude
    • Conrad M. RoseJeffrey J. Drude
    • G01S11/04G01S5/02G01S3/02
    • G01S11/04
    • An Angle of Arrival/Long Baseline Interferometer (AOA/LBI) passive ranging apparatus and method for emitter range determination can use any convenient airframe location for the two-antenna uncalibrated LBI baseline. This baseline has a theoretically unlimited length and does not require a specific SBI/LBI baseline ratio. Only a single initial AOA is required. Range partitions are formed along the single AOA. The emitter is assumed to lie in any of N range bins and the corresponding DOA (direction of arrival) unit vectors computed. Each of these DOA unit vectors is then used to predict the LBI phase differential and the N resolved LBI phases each drive a location estimator. The location estimator (filter) with consistent output provide the emitter range. The LBI range from these filters is used for subsequent DOA generation and ambiguity resolution.
    • 到达角度/长基线干涉仪(AOA / LBI)无源测距装置和发射器范围确定方法可以为双天线未校准的LBI基线使用任何方便的机身位置。 该基线在理论上具有无限长度,并且不需要特定的SBI / LBI基线比率。 只需要一个初始的AOA。 沿单一AOA形成范围分区。 假定发射极位于N个范围的任一个,并计算相应的DOA(到达方向)单位矢量。 然后将这些DOA单位向量中的每一个用于预测LBI相位差和N个解析的LBI相位,每个驱动位置估计器。 具有一致输出的位置估计器(滤波器)提供发射器范围。 这些滤波器的LBI范围用于随后的DOA生成和模糊度分辨。
    • 9. 发明授权
    • Method for single satellite geolocation of emitters using an ambiguous interferometer array
    • 使用模糊干涉仪阵列的发射器的单卫星地理定位方法
    • US08077088B2
    • 2011-12-13
    • US12198787
    • 2008-08-26
    • Conrad M. Rose
    • Conrad M. Rose
    • G01S5/04
    • G01S5/12G01S3/48G01S5/04
    • A method of locating a terrestrial emitter of electromagnetic radiation in the midst of a plurality of emitters in a satellite in orbit about the earth which utilizes a location estimation and location probability determination process with respect to each possible emitter site and its corresponding error region and then using both feedback and feed forward interaction between location and phase ambiguity resolution processes to generate resolved phase from emitter location, update emitter location or some or all of the emitters, and subsequently utilizing the probabilities thus determined to produce a single estimate of the desired emitter's location.
    • 一种在围绕地球轨道的卫星中的多个发射器的中间定位电磁辐射的地面发射体的方法,其利用关于每个可能的发射器位置及其对应的误差区域的位置估计和位置概率确定过程,然后 使用位置和相位模糊度分辨过程之间的反馈和前馈交互来产生来自发射器位置的分辨相位,更新发射器位置或一些或所有发射器,并且随后利用由此确定的概率来产生所需发射器位置的单个估计 。
    • 10. 发明授权
    • Augmented passive tracking of moving emitter
    • 增强移动发射器的被动跟踪
    • US07626538B2
    • 2009-12-01
    • US11923523
    • 2007-10-24
    • Conrad M. Rose
    • Conrad M. Rose
    • G01S13/88G01S13/00
    • G01S7/021G01S3/46G01S13/723G01S13/86
    • In one embodiment, the disclosure relates to a method for estimating and predicting a target emitter's kinematics, the method including the steps of: (a) passively sampling, at a first sampling rate, an emitter signal to obtain at least one passively measured signal attribute for estimating the target kinematics; (b) inputting the passively measured signal attribute to an estimator at a first sampling rate; (c) determining a radar duty cycle for active radar measurements as a multiple of the first sampling rate, the multiple defining a duration between radar transmissions; (d) directing a radar system to make active target measurements at the determined duty cycle; (e) inputting to the estimator the active target measurements at the determined duty cycle, while continuously inputting the passively measured signal attributes.
    • 在一个实施例中,本公开涉及一种用于估计和预测目标发射器运动学的方法,所述方法包括以下步骤:(a)以第一采样率被动采样发射器信号以获得至少一个被动测量的信号属性 用于估计目标运动学; (b)以第一采样率将被动测量的信号属性输入到估计器; (c)将主动雷达测量的雷达占空比确定为第一采样率的倍数,该倍数定义雷达传输之间的持续时间; (d)指导雷达系统在确定的占空比下进行主动目标测量; (e)在连续输入被动测量的信号属性的同时,以确定的占空比向估计器输入有效的目标测量值。