FIELD: satellite navigation for determining the vector of condition of users according to the signals of two mutually asynchronized systems. SUBSTANCE: receiver indicator uses antenna 1, receiver 2, reference generator 3, single-channel primary data processing unit, having pseudorandom sequence generator 5, frequency-code correlator 4, integrator unit 6 and radionavigational parameters measurement unit 7, interface unit 8, communication line signal level matching unit 9, navigational parameters vector determining unit 10, two internal storages 11, two permanent storages 12, 16, input-output unit 13, timer 14, indicator 17. EFFECT: enhanced reliability. 2 cl, 16 dwg
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Authors
Dates
1997-05-10—Published
1994-06-23—Filed