SPACE NAVIGATION SYSTEM AND METHOD Russian patent published in 2015 - IPC G01C21/24 

Abstract RU 2568937 C2

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

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RU 2 568 937 C2

Authors

Stepanov Valerij Viktorovich

Dates

2015-11-20Published

2014-05-13Filed