SU1412474A1 - Complex meter of coordinate of flying vehicle - Google Patents

Complex meter of coordinate of flying vehicle

Info

Publication number
SU1412474A1
SU1412474A1 SU4112080/09A SU4112080A SU1412474A1 SU 1412474 A1 SU1412474 A1 SU 1412474A1 SU 4112080/09 A SU4112080/09 A SU 4112080/09A SU 4112080 A SU4112080 A SU 4112080A SU 1412474 A1 SU1412474 A1 SU 1412474A1
Authority
SU
USSR - Soviet Union
Prior art keywords
navigation
range
radio
meter
receiver
Prior art date
Application number
SU4112080/09A
Other languages
Russian (ru)
Inventor
В.М. Лавриненко
Г.А. Николаев
Б.В. Пономаренко
Ю.Я. Поляков
С.П. Федотов
Р.С. Щербаков
С.В. Губкин
Original Assignee
В.М. Лавриненко
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by В.М. Лавриненко filed Critical В.М. Лавриненко
Priority to SU4112080/09A priority Critical patent/SU1412474A1/en
Application granted granted Critical
Publication of SU1412474A1 publication Critical patent/SU1412474A1/en

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  • Navigation (AREA)

Abstract

FIELD: radio navigation. SUBSTANCE: complex meter has self-contained navigation sensor 1, converter 2 of autonomous navigation data, airborne radio system 3 of short-range navigation incorporating navigation receiver 19 and unit measuring azimuth and range, converter 4 of radio engineering data, subtracters 5, 6, filter 7 composed of subtracter 8, multipliers 9, 12, 13, summator 10, delay unit 11, storages 14, 15, 16 and synchronizer 17, voltage-to-code converter 18, navigation receiver 19, unit 20 measuring azimuth and range. Navigation receiver 19 consists of input unit 21, amplifier 22 of azimuth intermediate frequency, former 23 of azimuthal pulse, amplifier 24 of range intermediate frequency and decoder 25. Self-contained navigation sensor 1 measures navigation parameters of movement of flying vehicle (vector of air speed and relative bearing). Radio navigation receiver 19 performs selection by frequency and duration of signals of radio beacon of airborne radio system of short-range navigation. Error of measurement of coordinate in self-contained navigation sensor 1 is determined in filter 7 with allowance for obtained data. In this case adaptation of meter of change of noise level across input of airborne equipment of system of short-range navigation is performed by control over gain factor of filter of meter with the aid of automatic regulation voltage of amplification of navigation receiver 19. EFFECT: increased accuracy of measurements. 1 dwg
SU4112080/09A 1986-08-09 1986-08-09 Complex meter of coordinate of flying vehicle SU1412474A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU4112080/09A SU1412474A1 (en) 1986-08-09 1986-08-09 Complex meter of coordinate of flying vehicle

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU4112080/09A SU1412474A1 (en) 1986-08-09 1986-08-09 Complex meter of coordinate of flying vehicle

Publications (1)

Publication Number Publication Date
SU1412474A1 true SU1412474A1 (en) 1995-05-27

Family

ID=60534015

Family Applications (1)

Application Number Title Priority Date Filing Date
SU4112080/09A SU1412474A1 (en) 1986-08-09 1986-08-09 Complex meter of coordinate of flying vehicle

Country Status (1)

Country Link
SU (1) SU1412474A1 (en)

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