METHOD OF DETERMINING POSITION OF NAVIGATION INFORMATION USER OBJECTS AND DEVICE FOR REALISING SAID METHOD Russian patent published in 2010 - IPC G01S5/14 

Abstract RU 2402786 C1

FIELD: physics.

SUBSTANCE: in a method of determining the position of a user object from navigation radio signals, where navigation parametres are determined - measurement of pseudorange and phase of the signal at pseudo-Doppler frequency from navigation radio signals of an orbital group of navigation spacecraft NKA1 of the GLONASS system and NKA2 of the GPS system, the user is sent basic navigation information and auxiliary information from which the position of the object is determined. Navigation radio signals are used in three frequency ranges L1, L2 and L3 for the GLONASS system and L5 for the GPS system respectively. Auxiliary information is supplemented with data on the state of the troposphere and parametres related to movement of the Earth in the solar system. Basic navigation information is generated onboard navigation spacecraft NKA1 using a network of ground-based base stations and a system of intersatellite communication and measurements.

EFFECT: more accurate determination of the position of a user object working in absolute mode to a level achieved using differential navigation systems.

2 cl, 1 dwg

Similar patents RU2402786C1

Title Year Author Number
METHOD OF IDENTIFICATION OF NAVIGATION SATELLITES PARAMETERS WITH COMPENSATION OF NAVIGATION RECEIVER ERRORS 2015
  • Akperov Imran Gurru Ogly
  • Kamenskij Vladislav Valerevich
  • Kramarov Sergej Olegovich
  • Lukasevich Viktor Ivanovich
  • Sokolov Sergej Viktorovich
RU2638411C2
METHOD AND SYSTEM FOR MULTIFREQUENCY POSITIONING IN SHIELDED SPACE 2013
  • Mikhajlenko Aleksandr L'Vovich
  • Medvedev Mikhail Jur'Evich
  • Babakov Valerij Nikolaevich
  • Penenko Aleksandr Petrovich
  • Sasaga Nikolaj Nikolaevich
RU2543521C1
METHOD OF IDENTIFYING PARAMETERS OF NAVIGATION SATELLITES 2015
  • Akperov Imran Gurruevich
  • Kamenskij Vladislav Valerevich
  • Kramarov Sergej Olegovich
  • Sokolov Sergej Viktorovich
  • Lukasevich Viktor Ivanovich
  • Tishshenko Evgenij Nikolaevich
RU2587666C1
APPLICATION OF TRIANGULAR METHODS OF MEASUREMENTS IN THE GLONASS SYSTEM 2015
  • Kalinin Boris Pavlovich
RU2669042C2
SATELLITE NAVIGATION SYSTEM FOR DETECTION OF OBJECT POSITION 1999
  • Vinogradov A.A.
  • Dvorkin V.V.
  • Sojuzov M.V.
  • Urlichich Ju.M.
RU2152050C1
SYSTEM FOR HIGH-ACCURACY LOCALIZATION OF OBJECTS- NAVIGATIONAL INFORMATION USERS BY NAVIGATIONAL RADIO SIGNALS WITH AUTHORIZED ACCESS IN REGIME OF DIFFERENTIAL CORRECTIONS 2000
  • Vinogradov A.A.
  • Dvorkin V.V.
  • Sojuzov M.V.
  • Urlichich Ju.M.
RU2161317C1
COORDINATE-INFORMATION SUPPORT METHOD FOR UNDERWATER MOBILE OBJECTS 2007
  • Chubykin Aleksej Alekseevich
  • Katenin Vladimir Aleksandrovich
RU2390098C2
METHOD FOR EPHEMERAL CONTROL OF SPACECRAFT GLOBAL NAVIGATION SATELLITE SYSTEM 2009
  • Strel'Nikov Sergej Vasil'Evich
RU2390730C1
METHOD OF PROBING IONOSPHERE, TROPOSPHERE, GEOLOGIC MOVEMENTS AND SET FOR IMPLEMENTING SAID METHOD 2011
  • Tertyshnikov Aleksandr Vasil'Evich
  • Pulinets Sergej Aleksandrovich
RU2502080C2
SIMULATOR OF RADIO NAVIGATION SIGNALS 2018
  • Grebennikov Andrej Vladimirovich
  • Krasnenko Sergej Sergeevich
  • Pichkalev Aleksandr Valerevich
  • Khazagarov Yurij Gennadevich
RU2697811C2

RU 2 402 786 C1

Authors

Dvorkin Vjacheslav Vladimirovich

Karutin Sergej Nikolaevich

Shilov Anatolij Evgen'Evich

Dates

2010-10-27Published

2009-10-01Filed