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SU1753833A1 - Airborne complex of satellite navigation - Google Patents

Airborne complex of satellite navigation

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Publication number
SU1753833A1
SU1753833A1 SU4880133/09A SU4880133A SU1753833A1 SU 1753833 A1 SU1753833 A1 SU 1753833A1 SU 4880133/09 A SU4880133/09 A SU 4880133/09A SU 4880133 A SU4880133 A SU 4880133A SU 1753833 A1 SU1753833 A1 SU 1753833A1
Authority
SU
USSR - Soviet Union
Prior art keywords
satellite navigation
unit
meters
determination
navigation system
Prior art date
Application number
SU4880133/09A
Other languages
Russian (ru)
Inventor
А.В. Комаров
С.И. Котяшкин
В.П. Майко
П.П. Рязанцев
Л.В. Шестопалов
Original Assignee
Научно-исследовательский и проектный институт "Океангеофизика"
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 Научно-исследовательский и проектный институт "Океангеофизика" filed Critical Научно-исследовательский и проектный институт "Океангеофизика"
Priority to SU4880133/09A priority Critical patent/SU1753833A1/en
Application granted granted Critical
Publication of SU1753833A1 publication Critical patent/SU1753833A1/en

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  • Position Fixing By Use Of Radio Waves (AREA)

Abstract

FIELD: determination of position of object. SUBSTANCE: complex includes two-frequency receiving indicator of low-orbit satellite navigation system incorporating aerial 1, two receivers 2, 3, two meters 4, 5 of Doppler frequency drift, encoder 6, frequency synthesizer 7, coordinate computer 8, receiving indicator of medium-orbit satellite navigation system involving aerial 9, n reception channels 10 and 11, n meters of pseudodistance 12, 13, unit 14 for extraction of navigational message, frequency synthesizer 15 and navigational computer 16 as well as reference generator 17, timer 18, unit 19 for input/output, display unit 20, former 21 of ionization coefficient, meter 22 of ionospheric delay and n adders 23 and 24. EFFECT: increased accuracy of determination of position thanks to real time measurement of ionospheric ionization. 3 cl, 2 dwg
SU4880133/09A 1990-10-01 1990-10-01 Airborne complex of satellite navigation SU1753833A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU4880133/09A SU1753833A1 (en) 1990-10-01 1990-10-01 Airborne complex of satellite navigation

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU4880133/09A SU1753833A1 (en) 1990-10-01 1990-10-01 Airborne complex of satellite navigation

Publications (1)

Publication Number Publication Date
SU1753833A1 true SU1753833A1 (en) 1994-06-15

Family

ID=60532780

Family Applications (1)

Application Number Title Priority Date Filing Date
SU4880133/09A SU1753833A1 (en) 1990-10-01 1990-10-01 Airborne complex of satellite navigation

Country Status (1)

Country Link
SU (1) SU1753833A1 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2419804C2 (en) * 2005-11-07 2011-05-27 Дзе Боинг Компани Methods and devices for navigation system with lower susceptibility to intended and unintended interferences

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2419804C2 (en) * 2005-11-07 2011-05-27 Дзе Боинг Компани Methods and devices for navigation system with lower susceptibility to intended and unintended interferences

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