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1. 发明申请

WO03096057A2 METHODS AND APPARATUS FOR MINIMUM COMPUTATION PHASE DEMODULATION 审中-公开
标题翻译：用于最小计算相位解析的方法和装置
公开(公告)号：WO03096057A2
公开(公告)日：2003-11-20
申请号：PCT/US0315919
申请日：2003-05-13
申请人： HONEYWELL INT INC
发明人： HAGER JAMES R , BURLET TODD R , JORDAN LAVELL
IPC分类号： G01S3/48 , G01S7/292 , G01S13/18 , G01S13/20 , G01S13/28 , G01S13/42 , G01S13/524 , G01S13/70 , G01S13/88 , G01S13/94 , G01S
CPC分类号： G01S7/292 , G01S3/48 , G01S13/18 , G01S13/20 , G01S13/288 , G01S13/42 , G01S13/524 , G01S13/70 , G01S13/882 , G01S13/94
摘要： A filter (304), includes a first order band pass filter configured to process non-zero amplitude gated radar return samples and process a portion of received zero amplitude return samples. The filter also calculates past filter outputs based on filter outputs generated during previous non-zero gated radar return samples.
摘要翻译：滤波器（304）包括被配置为处理非零幅度门控雷达返回样本并且处理接收的零幅度返回样本的一部分的第一阶带通滤波器。滤波器还可以根据先前非零门控雷达返回样本中生成的滤波器输出来计算过去的滤波器输出。

2. 发明申请

WO0159474A3 PRECISION RADAR ALTIMETER WITH TERRAIN FEATURE COORDINATE LOCATION CAPABILITY 审中-公开
标题翻译：具有特征功能的精密雷达测高仪坐标位置能力
公开(公告)号：WO0159474A3
公开(公告)日：2002-02-14
申请号：PCT/US0103229
申请日：2001-02-01
申请人： HONEYWELL INT INC
发明人： HAGER JAMES R , ALMSTED LARRY D , PETRICH CURTIS J
IPC分类号： B64D45/00 , G01S7/292 , G01S13/10 , G01S13/18 , G01S13/46 , G01S13/524 , G01S13/88 , G01S13/94
CPC分类号： G01S13/882 , G01S7/292 , G01S13/18 , G01S13/46 , G01S13/524 , G01S13/94
摘要： A radar altimeter for determining altitude of an air vehicle comprises a transmitter for transmitting radar signals toward the ground. A first and a second antenna receive reflected radar signals from the ground. A signal processor is coupled to the first and the second antennas. The signal processor includes filter means for rejecting signals other than signals reflected from a selected ground swath. The signal processor determines the above ground level altitude of the air vehicle based on the radar signals output from the filter means. A phase ambiguity resolution means resolves phase ambiguities that arise due to multiple wavelength separation of the first and the second antenna. The signal processor also determines the horizontal position of the highest point in the selected ground swath. In a preferred embodiment, the phase ambiguity resolution means comprises a third antenna spaced closely to the first antenna such that there are no phase ambiguities between the reflected radar signals received by the third antenna and the first antenna.
摘要翻译：用于确定空中交通工具的高度的雷达高度计包括用于向地面发射雷达信号的发射机。第一和第二天线从地面接收反射的雷达信号。信号处理器耦合到第一和第二天线。信号处理器包括滤波器装置，用于拒绝除了从所选地线所反射的信号之外的信号。信号处理器基于从过滤装置输出的雷达信号确定空中交通工具的上述地面高度。相位歧义解决方案解决由于第一和第二天线的多波长分离而产生的相位模糊度。信号处理器还确定所选接地线中最高点的水平位置。在优选实施例中，相位模糊度分辨装置包括与第一天线紧密相邻的第三天线，使得在由第三天线和第一天线接收的反射的雷达信号之间不存在相位模糊。

3. 发明申请

WO2005121831A3 METHODS AND SYSTEMS FOR ENHANCING ACCURACY OF TERRAIN AIDED NAVIGATION SYSTEMS 审中-公开
标题翻译：提高地形辅助导航系统精度的方法和系统
公开(公告)号：WO2005121831A3
公开(公告)日：2007-05-10
申请号：PCT/US2005019334
申请日：2005-06-02
申请人： HONEYWELL INT INC , HAGER JAMES R , ALMSTED LARRY D
发明人： HAGER JAMES R , ALMSTED LARRY D
IPC分类号： G01C21/00 , G01C21/26 , G01S13/00 , G01S13/86 , G01S13/88 , G06F19/00
CPC分类号： G01C21/005 , G01S5/0252 , G01S13/86 , G01S13/882
摘要： A navigation system (200) is described which includes a navigation processor (208), an inertial navigation unit (206) configured to provide a position solution to the navigation processor, and a digital elevation map (212). The described navigation system also includes a radar altimeter (50) having a terrain correlation processor (210) configured to receive map data from the digital elevation map and provide a position solution based on radar return data to the navigation processor. A map quality processor (202) within the navigation system is configured to receive map data from the digital elevation map and provide a map quality factor to the navigation processor which weights (256) the position solution from the terrain correlation processor according to the map quality factor and determines a position solution from the weighted terrain correlation processor position solution and the position solution from the inertial navigation unit.
摘要翻译：描述了包括导航处理器（208），被配置为向导航处理器提供位置解决方案的惯性导航单元（206）以及数字高程图（212）的导航系统（200）。所描述的导航系统还包括雷达高度计（50），其具有被配置为从数字高程图接收地图数据并且基于雷达返回数据向导航处理器提供位置解的地形相关处理器（210）。导航系统内的地图质量处理器（202）被配置为从数字高程地图接收地图数据，并向导航处理器提供地图质量因子，其根据地图质量从地形相关处理器加权（256）因子，并根据加权地形相关处理器位置解决方案和来自惯性导航单元的位置解决方案确定位置解决方案。

4. 发明申请

WO2005031386A3 RADAR ANTI-FADE SYSTEMS AND METHODS 审中-公开
标题翻译：雷达抗衰落系统和方法
公开(公告)号：WO2005031386A3
公开(公告)日：2005-06-02
申请号：PCT/US2004018098
申请日：2004-06-08
申请人： HONEYWELL INT INC , HAGER JAMES R , LAVELL JORDAN
发明人： HAGER JAMES R , LAVELL JORDAN
IPC分类号： G01S7/285 , G01S13/18 , G01S13/22 , G01S13/28 , G01S13/88
CPC分类号： G01S13/18 , G01S13/22 , G01S13/288 , G01S13/882
摘要： A method for suppressing ground return radar fading in a radar altimeter (10) is described. The method includes providing a radar gate width which corresponds to an area (140) that is smaller than an antenna illumination area being impinged by transmissions of the radar altimeter, dithering the radar gate viewing area (102) within the antenna illumination area being impinged by transmissions of the radar altimeter, and taking radar return samples with the radar altimeter.
摘要翻译：描述了一种用于抑制雷达高度计（10）中的地面返回雷达衰落的方法。该方法包括提供雷达门宽度，该雷达门宽度对应于小于由雷达高度计的传输所照射的天线照明区域的区域（140），使天线照明区域内的雷达门观察区域（102）抖动雷达高度计的发射，以及雷达高度计的雷达返回样本。

5. 发明申请

WO0196901A2 LOW PROBABILITY OF INTERCEPT COHERENT RADAR ALTIMETER 审中-公开
标题翻译：干涉相干雷达高度计的低概率
公开(公告)号：WO0196901A2
公开(公告)日：2001-12-20
申请号：PCT/US0118833
申请日：2001-06-11
申请人： HONEYWELL INT INC
发明人： HAGER JAMES R , KEUPER JOHN H , PETRICH CURTIS J
IPC分类号： G01S7/03 , G01S7/40 , G01S13/02 , G01S13/26 , G01S13/88 , G01S13/00
CPC分类号： G01S7/4004 , G01S7/032 , G01S7/4008 , G01S13/26 , G01S13/882 , G01S2013/0281
摘要： A radar altimeter for determining altitude of an air vehicle with respect to ground comprises a digital sequencer for digitally modulating a first signal. A transmitter coupled to the digital sequencer transmits a radar signal including the modulated first signal toward the ground. A receiver receives a reflected radar signal from the ground. The received radar signal includes the modulated first signal. A digitizer coupled to the receiver generates digital samples of the modulated first signal. A digital signal processor coupled to the digitizer receives digital samples of the modulated first signal from the digitizer, demodulates the received digital samples, processes the demodulated digital samples and outputs altitude data based on the demodulated digital samples.
摘要翻译：用于确定空中交通工具相对于地面的高度的雷达高度计包括用于数字调制第一信号的数字定序器。耦合到数字定序器的发射器将包括经调制的第一信号的雷达信号发射到地面。接收机从地面接收反射的雷达信号。所接收的雷达信号包括经调制的第一信号。耦合到接收器的数字转换器产生调制的第一信号的数字样本。耦合到数字转换器的数字信号处理器从数字转换器接收经调制的第一信号的数字采样，解调所接收的数字采样，处理解调的数字采样并基于解调的数字样本输出高度数据。

6. 发明申请

WO2005121831A8 METHODS AND SYSTEMS FOR ENHANCING ACCURACY OF TERRAIN AIDED NAVIGATION SYSTEMS 审中-公开
标题翻译：增强导航导航系统精度的方法与系统
公开(公告)号：WO2005121831A8
公开(公告)日：2007-03-01
申请号：PCT/US2005019334
申请日：2005-06-02
申请人： HONEYWELL INT INC , HAGER JAMES R , ALMSTED LARRY D
发明人： HAGER JAMES R , ALMSTED LARRY D
IPC分类号： G01S13/00 , G01C21/00 , G01C21/26 , G01S13/86 , G01S13/88 , G06F19/00
CPC分类号： G01C21/005 , G01S5/0252 , G01S13/86 , G01S13/882
摘要： A navigation system (200) is described which includes a navigation processor (208), an inertial navigation unit (206) configured to provide a position solution to the navigation processor, and a digital elevation map (212). The described navigation system also includes a radar altimeter (50) having a terrain correlation processor (210) configured to receive map data from the digital elevation map and provide a position solution based on radar return data to the navigation processor. A map quality processor (202) within the navigation system is configured to receive map data from the digital elevation map and provide a map quality factor to the navigation processor which weights (256) the position solution from the terrain correlation processor according to the map quality factor and determines a position solution from the weighted terrain correlation processor position solution and the position solution from the inertial navigation unit.
摘要翻译：描述了一种导航系统（200），其包括导航处理器（208），被配置为向导航处理器提供位置解决方案的惯性导航单元（206）和数字高程图（212）。所描述的导航系统还包括具有地形相关处理器（210）的雷达高度计（50），其被配置为从数字高程图接收地图数据，并且向导航处理器提供基于雷达返回数据的位置解。导航系统内的地图质量处理器（202）被配置为从数字高程图接收地图数据，并向导航处理器提供地图品质因子，该导航处理器根据地图质量权重（256）来自地形相关处理器的位置解并从加权地形相关处理器位置解决方案和来自惯性导航单元的位置解决方案确定位置解。

7. 发明申请

WO2006112884A3 METHODS AND SYSTEMS FOR CONTROLLING A HEIGHT OF MUNITION DETONATION 审中-公开
标题翻译：用于控制火焰爆发高度的方法和系统
公开(公告)号：WO2006112884A3
公开(公告)日：2007-02-01
申请号：PCT/US2005040951
申请日：2005-11-12
申请人： HONEYWELL INT INC , HAGER JAMES R , REILLY TIMOTHY J , BACKES GLEN
发明人： HAGER JAMES R , REILLY TIMOTHY J , BACKES GLEN
IPC分类号： F42C13/04
CPC分类号： F42C13/04 , F42C13/047 , G01S7/038 , G01S13/882
摘要： A unit (12) is described that is configured to control detonation of a munition (10) such that the munition is detonated at a desired altitude. The unit includes a radar transmitter, a radar receiver (64) that includes a radar range gate (76), and a sequencer (90). The sequencer is configured to receive a detonation altitude (92) and set the range gate based on the received detonation altitude. The unit is also configured to output a detonation signal when radar return pulses received by the receiver aligned with gate delay pulses (122) from the range gate.
摘要翻译：描述了一个单元（12），其被配置为控制弹药（10）的爆炸，使得弹药以期望的高度被引爆。该单元包括雷达发射器，包括雷达测距门（76）的雷达接收器（64）和定序器（90）。定序器被配置为接收爆震高度（92），并且基于接收到的引爆高度来设置范围门。该单元还被配置为当由接收器接收的雷达返回脉冲与来自范围门的门延迟脉冲（122）对准时，输出引爆信号。

8. 发明申请

WO2006085951A3 SYSTEM AND METHODS FOR GUIDING MUNITIONS 审中-公开
标题翻译：指导弹药的系统和方法
公开(公告)号：WO2006085951A3
公开(公告)日：2006-10-05
申请号：PCT/US2005021850
申请日：2005-06-17
申请人： HONEYWELL INT INC , THOMAS STEVE H , HAGER JAMES R
发明人： THOMAS STEVE H , HAGER JAMES R
IPC分类号： F41G7/00 , F41G7/22 , F41G9/00 , F42B10/60 , F42B10/62 , G01S3/56 , G01S13/42
CPC分类号： F41G7/222 , G01S3/56 , G01S13/422
摘要： A method of guiding a munition (20) to a target (10) transmitting one or more signals is described. The method includes configuring the munition with a radio frequency receiver (60), an antenna (62) for the receiver mounted such that a main beam of the antenna pattern (40) for the antenna is offset from a line of flight axis (42) of the munition by an angle (26) and configuring the munition to rotate along an axis substantially similar to the line of flight axis of the munition. The method also includes configuring the munition to process signals received at the antenna, wherein heading changes of the munition, the angle of the main beam of the antenna from the line of flight axis, and the rotation of the munition result in the received signals having amplitude variations. Directional corrections are: generated for the munition to direct the munition towards the target based on amplitude variations in the received signals.
摘要翻译：描述了将军火（20）引导到发送一个或多个信号的目标（10）的方法。该方法包括用射频接收器（60）配置弹药，安装接收器的天线（62），使得天线的天线图案（40）的主射束偏离飞行轴线（42）的一条线，以一定角度（26）弹药并配置弹药沿着基本上类似于弹药的飞行轴线的轴线旋转。该方法还包括配置弹药以处理在天线处接收到的信号，其中弹药的方位改变，天线的主束的角度与飞行轴线的角度以及弹药的旋转导致接收到的信号具有幅度变化。定向校正是：为弹药根据接收信号的幅度变化将弹药引向目标而产生。

9. 发明专利

CA2527725A1 RADAR ANTI-FADE SYSTEMS AND METHODS 未知
公开(公告)号：CA2527725A1
公开(公告)日：2005-04-07
申请号：CA2527725
申请日：2004-06-08
申请人： HONEYWELL INT INC
发明人： LAVELL JORDAN , HAGER JAMES R
IPC分类号： G01S13/18 , G01S7/285 , G01S13/22 , G01S13/28 , G01S13/88
摘要： A method for suppressing ground return radar fading in a radar altimeter (10 ) is described. The method includes providing a radar gate width which corresponds to an area (140) that is smaller than an antenna illumination ar ea being impinged by transmissions of the radar altimeter, dithering the radar gate viewing area (102) within the antenna illumination area being impinged by transmissions of the radar altimeter, and taking radar return samples with t he radar altimeter.

10. 发明专利

CA2485699A1 DETERMINING AN ANGLE TO A TARGET USING INTERFEROMETRY 未知
公开(公告)号：CA2485699A1
公开(公告)日：2003-11-20
申请号：CA2485699
申请日：2003-05-13
申请人： HONEYWELL INT INC
发明人： BURLET TODD R , HAGER JAMES R , JORDAN LAVELL
IPC分类号： G01S13/50 , G01S3/48 , G01S7/292 , G01S13/18 , G01S13/20 , G01S13/28 , G01S13/42 , G01S13/524 , G01S13/70 , G01S13/88 , G01S13/935 , G01S7/32 , G01S13/46 , G01S13/94
摘要： A method for processing radar return data to determine a physical angle, in aircraft body coordinates to a target, is disclosed. The radar return data inludes a phase difference between radar return data received at an ambiguou s radar channel (226) and a left radar channel (224), a phase difference betwe en radar return data received at a right radar channel (228) and an ambiguous radar channel (226), and a phase defference between radar return data receiv ed at a rigth radar channel (228) and a left radar channel (224). The method includes adjusting a phase bias (570, 572, 574) for the three phase differences, resolving phase ambiguities (576) between the three Phase differences to provide a signal, and filtering the signal (578) to provide a physical angle to the target in aircraft body coodinates.

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