会员体验
专利管家(专利管理)
工作空间(专利管理)
风险监控(情报监控)
数据分析(专利分析)
侵权分析(诉讼无效)
联系我们
交流群
官方交流:
QQ群: 891211   
微信请扫码    >>>
现在联系顾问~
热词
    • 2. 发明申请
    • Daytime stellar imager
    • 白天恒星成像仪
    • US20060085129A1
    • 2006-04-20
    • US11106744
    • 2005-04-15
    • Mikhail BelenkiiDonald BrunsVincent RyeTimothy Brinkley
    • Mikhail BelenkiiDonald BrunsVincent RyeTimothy Brinkley
    • G01C21/00
    • G01C21/025
    • An automatic celestial navigation system for navigating both night and day by observation of K-band or H-band infrared light from multiple stars. A preferred embodiment uses three telescopes with each of the three telescopes rigidly mounted with respect to each other and rigidly mounted on a movable platform such as a ship or airplane with each telescope being directed at a substantially different portion of sky. Telescope optics focuses, onto the pixel array of a sensor, H-band or K-band light from stars in the field of view of each telescope. The system also includes an inclinometer, an accurate timing device and a computer processor having access to cataloged infrared star charts. The processor is programmed with special algorithms to use image data from the infrared sensors, inclination information from the inclinometer, time information from the timing device and the cataloged star charts information to determine positions of the platform. At least two telescopes pointed far enough from the sun detect stars. Direction information from two stars is needed for locating the platform with respect to the celestial sphere. The computer is also preferably programmed to use this celestial position information to calculate latitude, longitude and absolute azimuth, all of which may be displayed on a display device such as a monitor. In a preferred embodiment each of the three telescopes are fixed on a moving ship and views a 0.5×0.4 degree region of the sky for H-band starlight from stars with brightness greater than 6.4 H-band magnitude. Located stars are then compared with star positions from the star catalog within a selected 5×5 degree region of the sky. A correlation of the data from the three telescopic measurements determines the position of the ship to a precision of 30 meters.
    • 通过观察来自多颗恒星的K波段或H波段红外光的自动天体导航系统,用于夜间和日间的导航。 优选实施例使用三个望远镜,三个望远镜中的每一个相对于彼此刚性地安装并且刚性地安装在诸如船或飞机的可移动平台上,其中每个望远镜被引导到天空的基本上不同的部分。 望远镜光学器件在每个望远镜的视野中聚焦到传感器的像素阵列上,来自恒星的H波段或K波段光。 该系统还包括倾斜计,准确的定时装置和具有访问编目红外星图的计算机处理器。 处理器采用特殊算法编程,以使用红外传感器的图像数据,倾斜仪的倾斜信息,定时装置的时间信息和编目的星形图信息来确定平台的位置。 至少有两颗望远镜指向远离太阳的星星。 需要来自两颗恒星的方向信息来定位平台相对于天球。 计算机还优选地被编程为使用该天体位置信息来计算纬度,经度和绝对方位角,所有这些都可以显示在诸如监视器的显示装置上。 在优选实施例中,三个望远镜中的每一个都固定在移动的船上,并且对于具有大于6.4H波段幅度的亮度的恒星的H波段星光,观察天空的0.5×0.4度的区域。 然后,将星星与天空中选定的5x5度区域内的星形目录进行比较。 来自三个望远镜测量数据的相关性确定了船舶的位置,精度为30米。
    • 3. 发明申请
    • Portable celestial compass
    • 便携式天文罗盘
    • US20120116711A1
    • 2012-05-10
    • US12283785
    • 2008-09-15
    • Donald BrunsTimothy Brinkley
    • Donald BrunsTimothy Brinkley
    • G01C17/34G06F15/00
    • G01C17/34G01C21/025
    • A portable celestial compass (PCC) that provides a new multi-functional capability for high precision target localization. The battery-powered PCC is built around US Army's M-25 stabilized binocular and includes a miniature eye-safe laser range finder, a gyro stabilized binocular, a 3-axis tilt compensated digital compass, and a built-in specialized chip with star catalog and software for target AZ/EL determination and sight reduction. A gyro stabilized binocular rejects up to 98% of image motion caused by hand tremor and platform vibration. Laser rangefinder has the accuracy of ±2 m at 5 km range. The PCC uses celestial objects as absolute references for target azimuth and elevation determination. The azimuth and elevation accuracy is 2 mrad, or 10 m at 5 km range, which is by a factor of up to 5 better than that for a magnetic compass.
    • 便携式天文罗盘(PCC),为高精度目标定位提供了新的多功能能力。 电池供电的PCC是围绕美国陆军的M-25稳定双目镜建立的,包括一个微型眼睛安全激光测距仪,一个陀螺稳定双目镜,一个3轴倾斜补偿数字罗盘,以及一个内置专用芯片,具有星级目录 和用于目标AZ / EL测定和视力降低的软件。 陀螺稳定的双目可以抑制由手震和平台振动造成的图像运动的98%。 激光测距仪在5公里范围内的精度为±2米。 PCC使用天体作为目标方位和仰角确定的绝对参考。 方位角和仰角精确度为2 mrad,或5 m,范围为5 m,比磁罗盘高5倍。
    • 4. 发明申请
    • Miniature celestial direction detection system
    • 微型天体方向检测系统
    • US20100283840A1
    • 2010-11-11
    • US12583776
    • 2009-08-25
    • Mikhail BelenkiiDonald BrunsTimothy Brinkley
    • Mikhail BelenkiiDonald BrunsTimothy Brinkley
    • H04N7/18G01S19/42G01C3/04
    • G01S19/14G01C21/02G01S3/7867H04N7/18
    • A celestial direction finding system. The system includes an inclinometer, at least one camera for imaging both the daytime sky and the nighttime sky and a computer programmed with a sun, moon and star catalog and algorithms for automatically determining directions based on positions of celestial bodies imaged by at least one camera and incline positions measured by the inclinometer. In a preferred embodiment all of the above features are combined in a single battery operated miniature celestial direction finding module. Geographical positions of nearby objects can be determined with the addition of a rangefinder and knowledge of the geographical position of the camera. The geographical position of the system in preferred embodiments can be determined with the addition of a GPS unit.
    • 天体测向系统。 该系统包括倾斜仪,用于对白天和夜间空间进行成像的至少一个相机和具有太阳,月亮和星号目录的计算机以及基于由至少一个照相机成像的天体的位置自动确定方向的算法 并倾斜测量仪倾斜位置。 在优选实施例中,所有上述特征组合在单个电池操作的微型天体测向模块中。 可以通过添加测距仪和相机的地理位置知识来确定附近物体的地理位置。 可以通过添加GPS单元来确定优选实施例中的系统的地理位置。
    • 6. 发明申请
    • Celestial weapons orientation measuring system
    • 天体武器导向测量系统
    • US20120021385A1
    • 2012-01-26
    • US12586813
    • 2009-09-28
    • Mikhail BelenkiiDonald BrunsTimothy Brinkley
    • Mikhail BelenkiiDonald BrunsTimothy Brinkley
    • F41G3/26
    • G09B27/00F41G3/26
    • A celestial weapons orientation measuring system. The system includes a miniature celestial direction detection device. The device includes an inclinometer, a camera for imaging at least one celestial object and a processor programmed with a celestial catalog providing known positions at specific times of at least one celestial object and algorithms for automatically calculating target direction information based on the inclination of the system as measured by the inclinometer and the known positions of the celestial object as provided by the celestial catalog and as imaged by the camera. Similar to the training technique discussed in the background section, the pretend enemy wears a GPS detector and transmitter, and a computer system is preferably provided which determines when a trigger-pull results in a “casualty”. Preferred embodiments also include an inertial navigation sensor including a magnetic compass and a memory-based optical navigation system that permits continued operation on cloudy days and even in certain in-door environments.
    • 天体武器导向测量系统。 该系统包括微型天体方向检测装置。 该装置包括倾斜计,用于对至少一个天体成像进行成像的照相机和在天体目录中编程的处理器,其在至少一个天体的特定时间提供已知位置,并且基于系统的倾斜自动计算目标方向信息的算法 如通过倾斜仪测量的,并且由天体目录提供的天体的已知位置以及通过照相机成像的天体的已知位置。 与背景技术中讨论的训练技术类似,伪装的敌人戴上GPS检测器和发射器,并且优选地提供计算机系统,其确定何时触发拉动导致“伤员”。 优选实施例还包括惯性导航传感器,其包括磁罗盘和基于存储器的光学导航系统,其允许在阴天甚至在某些室内环境中继续操作。
    • 7. 发明申请
    • Daytime stellar imager
    • US20070038374A1
    • 2007-02-15
    • US11141526
    • 2005-05-31
    • Mikhail BelenkiiDonald BrunsVincent RyeTimothy Brinkley
    • Mikhail BelenkiiDonald BrunsVincent RyeTimothy Brinkley
    • G05D1/08G01C21/00
    • G01C21/025
    • An automatic celestial navigation system for navigating both night and day by observation of K-band or H-band infrared light from multiple stars. In a first set of preferred embodiments three relatively large aperture telescopes are rigidly mounted on a movable platform such as a ship or airplane with each telescope being directed at a substantially different portion of sky. Embodiments in this first set tend to be relatively large and heavy, such as about one cubic meter and about 60 pounds. In a second set of preferred embodiments one or more smaller aperture telescopes are pivotably mounted on a movable platform such as a ship, airplane or missile so that the telescope or telescopes can be pivoted to point toward specific regions of the sky. Embodiments of this second set are mechanically more complicated than those of the first set, but are much smaller and lighter and are especially useful for guidance of aircraft and missiles. Telescope optics focus (on to a pixel array of a sensor) H-band or K-band light from one or more stars in the field of view of each telescope. Each system also includes an inclinometer, an accurate timing device and a computer processor having access to catalogued infrared star charts. The processor for each system is programmed with special algorithms to use image data from the infrared sensors, inclination information from the inclinometer, time information from the timing device and the catalogued star charts information to determine positions of the platform. Direction information from two stars is needed for locating the platform with respect to the celestial sphere. The computer is also preferably programmed to use this celestial position information to calculate latitude and longitude which may be displayed on a display device such as a monitor or used by a guidance control system. These embodiments are jam proof and insensitive to radio frequency interference. These systems provide efficient alternatives to GPS when GPS is unavailable and can be used for periodic augmentation of inertial navigation systems.
    • 10. 发明授权
    • Celestial weapons orientation measuring system
    • 天体武器导向测量系统
    • US08597025B2
    • 2013-12-03
    • US12586813
    • 2009-09-28
    • Mikhail BelenkiiDonald BrunsTimothy Brinkley
    • Mikhail BelenkiiDonald BrunsTimothy Brinkley
    • F41G3/26
    • G09B27/00F41G3/26
    • A celestial weapons orientation measuring system. The system includes a miniature celestial direction detection device. The device includes an inclinometer, a camera for imaging at least one celestial object and a processor programmed with a celestial catalog providing known positions at specific times of at least one celestial object and algorithms for automatically calculating target direction information based on the inclination of the system as measured by the inclinometer and the known positions of the celestial object as provided by the celestial catalog and as imaged by the camera. Similar to the training technique discussed in the background section, the pretend enemy wears a GPS detector and transmitter, and a computer system is preferably provided which determines when a trigger-pull results in a “casualty”. Preferred embodiments also include an inertial navigation sensor including a magnetic compass and a memory-based optical navigation system that permits continued operation on cloudy days and even in certain in-door environments.
    • 天体武器导向测量系统。 该系统包括微型天体方向检测装置。 该装置包括倾斜计,用于对至少一个天体成像进行成像的照相机和在天体目录中编程的处理器,其在至少一个天体的特定时间提供已知位置,并且基于系统的倾斜自动计算目标方向信息的算法 如通过倾斜仪测量的,并且由天体目录提供的天体的已知位置以及通过照相机成像的天体的已知位置。 与背景技术中讨论的训练技术类似,伪装的敌人戴上GPS检测器和发射器,并且优选地提供计算机系统,其确定何时触发拉动导致“伤员”。 优选实施例还包括惯性导航传感器,其包括磁罗盘和基于存储器的光学导航系统,其允许在阴天甚至在某些室内环境中继续操作。