FIELD: radio engineering, communication.
SUBSTANCE: system has a space segment in form of navigation spacecraft, a transponder mounted on the mobile object and a ground segment in form of a ground measuring station. The transponder has a navigation spacecraft signal receiver, a carrier frequency converter and a relayed signal transmitter. The ground measuring station has a transponder signal receiving and processing unit, a unit for calculating coordinates of the transponder, as well as a correcting unit and a navigation spacecraft signal receiving and processing unit. The correcting unit has a unit for calculating ionospheric delay and a unit for calculating ephemeral-time support error of the navigation spacecraft, a weather data unit, an ionosphere data unit and a transponder position pre-calculating unit.
EFFECT: eliminating restrictions on a navigation coverage area with differential accuracy mode in conditions of providing radio communication from a transponder mounted on an object to a ground measuring station for any motion path of the mobile object.
3 dwg
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Authors
Dates
2013-08-20—Published
2012-03-27—Filed