NAVIGATION SYSTEM OF FLYING VEHICLE Russian patent published in 1994 - IPC

FIELD: computer technology. SUBSTANCE: system has radiolocation unit 1, current data memory unit 2, data distributor 3, group signals average intensity evaluation formers 4; the formers have divider 5, OR gates unit 6, register 7, commutator 8, adder 9, delay elements unit 10, commutators 11 and 12; multiplier 13, commutator 14, OR gates unit 15, register 16, multiplier 17, commutator 18, OR gates unit 19, commutator 20, delay elements unit 21, commutator 22, OR gates unit 23, register 24 and multiplier 25. System also has adder 26, log converter 27, divider 28, subtracter 29, coordinate former 30, inertial navigation unit 31, adder 32, log converter 33, divider 34, standard memory unit 35, trigger 36, synchronization unit 37, address former 38, pulse former 39, AND gate 40, counter 41, decoders 42 and 43, register 44, commutators 45 and 46, comparison units 47 and 48, trigger 49, register 50, commutators 52 and 51, trigger 53, register 54, group counters 55. EFFECT: improved precision of measurement of location. 4 dwg