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RU123176U8 - SYSTEM OF DETERMINING THE LOCATION OF THE NAVIGATION SPACE VEHICLE - Google Patents

SYSTEM OF DETERMINING THE LOCATION OF THE NAVIGATION SPACE VEHICLE Download PDF

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Publication number
RU123176U8
RU123176U8 RU2011131302/07U RU2011131302U RU123176U8 RU 123176 U8 RU123176 U8 RU 123176U8 RU 2011131302/07 U RU2011131302/07 U RU 2011131302/07U RU 2011131302 U RU2011131302 U RU 2011131302U RU 123176 U8 RU123176 U8 RU 123176U8
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RU
Russia
Prior art keywords
navigation
ground
feeder device
beacons
radio signals
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RU2011131302/07U
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Russian (ru)
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RU123176U1 (en
Inventor
Юрий Матэвич Урличич
Вячеслав Владимирович Дворкин
Сергей Николаевич Карутин
Владимир Петрович Иванов
Original Assignee
Открытое акционерное общество "Российская корпорация ракетно-космического приборостроения и информационных систем" (ОАО "Российские космические системы")
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Priority to RU2011131302/07U priority Critical patent/RU123176U8/en
Application granted granted Critical
Publication of RU123176U1 publication Critical patent/RU123176U1/en
Publication of RU123176U8 publication Critical patent/RU123176U8/en

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Abstract

1. Система определения местоположения навигационного космического аппарата состоит из орбитальной группировки навигационных космических аппаратов, связанной двухсторонней связью с наземными опорными автономными маяками, которые связаны с наземным центром управления системой, при этом каждый навигационный космический аппарат состоит из последовательно соединенных приемного антенно-фидерного устройства, бортового приемника навигационных сигналов, бортового цифрового вычислительного комплекса, бортового источника навигационного сигнала и передающего антенно-фидерного устройства, а каждый наземный опорный автономный маяк состоит из последовательно соединенных приемного антенно-фидерного устройства, приемника навигационных сигналов, цифрового вычислительного комплекса, источника навигационного сигнала и передающего антенно-фидерного устройства.2. Система по п.1, в которой наземные опорные автономные маяки формируют навигационные радиосигналы с использованием навигационных радиосигналов НКА в трех частотных диапазонах L1, L2 и L3 для системы ГЛОНАСС и L1, L2 и L5 для системы GPS соответственно.3. Система по п.1, в которой наземные опорные автономные маяки излучают навигационные радиосигналы в одном частотном диапазоне.4. Система по п.1, в которой наземный центр управления системой периодически рассчитывает координаты фазовых центров приемных и передающих антенн наземных опорных автономных маяков.1. The positioning system of the navigation spacecraft consists of an orbital constellation of navigation spacecraft connected by two-way communication with ground-based reference autonomous beacons that are connected to the ground control center of the system, with each navigation spacecraft consisting of a series-connected receiving antenna-feeder device receiver of navigation signals, on-board digital computer complex, on-board source of navigation a signal and a transmitting antenna-feeder device, and each ground-based reference autonomous beacon consists of a series-connected receiving antenna-feeder device, a receiver of navigation signals, a digital computer complex, a source of a navigation signal and a transmitting antenna-feeder device. 2. The system according to claim 1, in which the ground-based reference autonomous beacons generate navigation radio signals using navigation radio signals of the satellite in the three frequency ranges L1, L2 and L3 for the GLONASS system and L1, L2 and L5 for the GPS system, respectively. The system according to claim 1, in which the ground reference autonomous beacons emit navigation radio signals in the same frequency range. The system according to claim 1, in which the ground control center of the system periodically calculates the coordinates of the phase centers of the receiving and transmitting antennas of the ground reference autonomous beacons.

RU2011131302/07U 2011-07-26 2011-07-26 SYSTEM OF DETERMINING THE LOCATION OF THE NAVIGATION SPACE VEHICLE RU123176U8 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2011131302/07U RU123176U8 (en) 2011-07-26 2011-07-26 SYSTEM OF DETERMINING THE LOCATION OF THE NAVIGATION SPACE VEHICLE

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Application Number Priority Date Filing Date Title
RU2011131302/07U RU123176U8 (en) 2011-07-26 2011-07-26 SYSTEM OF DETERMINING THE LOCATION OF THE NAVIGATION SPACE VEHICLE

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RU123176U1 RU123176U1 (en) 2012-12-20
RU123176U8 true RU123176U8 (en) 2014-04-20

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2669042C2 (en) * 2015-06-09 2018-10-05 Борис Павлович Калинин Application of triangular methods of measurements in the glonass system

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2698159C1 (en) * 2019-05-06 2019-08-22 Акционерное общество "Российская корпорация ракетно-космического приборостроения и информационных систем" (АО "Российские космические системы") System for assessing the stability of a satellite positioning system, for example a glonass system, to unfavorable external effects

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2669042C2 (en) * 2015-06-09 2018-10-05 Борис Павлович Калинин Application of triangular methods of measurements in the glonass system

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