发明名称 SPACE NAVIGATION SYSTEM AND METHOD
摘要 FIELD: physics.SUBSTANCE: method comprises reception and spectral analysis of signals from a sensitive element, detecting signals received from different radio pulsars, identification thereof on an electronic map of the starry sky in a computing device and calculating the latitude and longitude of the observation point. The space navigation system comprises a sensitive element, a computing device, a memory unit with an electronic map (database) of pulsars, data cables and a latitude and longitude indicator, a sensitive element tilt sensor, wherein the sensitive element is in the form of a superweak radiation sensor having an omnipattern.EFFECT: broader functional capabilities.2 cl, 3 dwg
申请公布号 RU2568937(C2) 申请公布日期 2015.11.20
申请号 RU20140119357 申请日期 2014.05.13
申请人 STEPANOV VALERIJ VIKTOROVICH 发明人 STEPANOV VALERIJ VIKTOROVICH
分类号 G01C21/24 主分类号 G01C21/24
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