METHOD AND SYSTEM FOR IMPROVING ACCURACY OF DETERMINING LOCATION OF GLOBAL NAVIGATION SATELLITE SYSTEM CONSUMERS BY DIGITAL MARKING OF ROAD NETWORK SECTIONS Russian patent published in 2017 - IPC G01S19/42 

Abstract RU 2633093 C1

FIELD: physics.

SUBSTANCE: methods are based on the fact that in a local area of space, consumers who determine their location along the working constellation of the navigation system will have the same errors associated with the movement of satellites and the propagation of radio signals. In other words, at each instant they will have approximately the same corrective amendments due to the inaccuracy of satellite orbits and the condition for the propagation of radio signals. Compensation of these amendments will increase the accuracy of determining the location of consumers, leaving only individual errors for each device, in particular, multipath in the propagation of radio signals and internal receiver noise.

EFFECT: increasing the accuracy of determining the coordinates of single-frequency navigation receivers built into user mobile devices and not having the technical capabilities to obtain and apply corrective amendments from various existing differential subsystems.

13 cl, 4 dwg

Similar patents RU2633093C1

Title Year Author Number
METHOD FOR DETERMINATION OF OBJECT RELATIVE COORDINATES WITH SURVEY TO ARBITRARY POINT OF SPACE AND SYSTEM FOR ITS REALIZATION 2004
  • Urlichich Ju.M.
  • Dvorkin V.V.
  • Vinogradov A.A.
  • Averin S.V.
RU2253128C1
METHOD OF DETERMINATION OF VECTOR OF STATE OF MOBILE OBJECT WITH THE AID OF NAVIGATIONAL SPACECRAFTS OF SPACE NAVIGATION SYSTEM 1994
  • Mashkov A.V.
  • Pudlovskij V.B.
RU2070315C1
METHOD AND APPARATUS FOR CONTROLLING THE INTEGRITY OF MEASUREMENTS OF THE ON-BOARD EQUIPMENT OF THE GLOBAL NAVIGATION SATELLITE SYSTEM (GNSS) APPLYING MEASUREMENTS OF A SHORT-RANGE NAVIGATION RADIO SYSTEM AND PSEUDO SATELLITES 2021
  • Veremeenko Konstantin Konstantinovich
  • Zimin Roman Iurevich
RU2778093C1
METHOD FOR HIGH-PRECISION MEASUREMENT OF AIRCRAFT TRAJECTORY COORDINATES IN FLIGHT INVESTIGATIONS ON LONG ROUTES 2008
  • Kopylov Igor' Anatol'Evich
  • Polikarpov Valerij Georgievich
  • Padenko Viktor Mikhajlovich
  • Kharin Evgenij Grigor'Evich
  • Kopelovich Vladimir Abovich
  • Kalinin Jurij Ivanovich
  • Saparina Tat'Jana Petrovna
  • Frolkina Ljudmila Veniaminovna
  • Stepanova Svetlana Jur'Evna
RU2393430C1
METHOD OF CONTROLLING INTEGRITY OF WIDE-AREA DIFFERENTIAL SUBSYSTEMS OF SATELLITE RADIO NAVIGATION SYSTEMS 2007
  • Dem'Janov Vladislav Vladimirovich
  • Gamajunov Il'Ja Fedorovich
RU2361231C1
METHOD OF MEASURING RELATIVE POSITION OF OBJECTS FROM GLOBAL NAVIGATION SATELLITE SYSTEM SIGNALS 2015
  • Zhodzishskij Aleksandr Isaakovich
  • Nesterov Oleg Valeryanovich
RU2592077C1
METHOD OF FORWARD DIFFERENTIAL ERROR CORRECTION OF DETERMINING USERS COORDINATES OF MID-ORBITAL SATELLITE NAVIGATION SYSTEMS 2007
  • Dem'Janov Vladislav Vladimirovich
  • Gamajunov Il'Ja Fedorovich
RU2359283C2
SATELLITE NAVIGATION SYSTEM FOR DETECTION OF OBJECT POSITION 1999
  • Vinogradov A.A.
  • Dvorkin V.V.
  • Sojuzov M.V.
  • Urlichich Ju.M.
RU2152050C1
METHOD OF DETERMINING MUTUAL POSITION OF OBJECTS BY SIGNALS OF GLOBAL NAVIGATION SATELLITE SYSTEMS 2016
  • Zhodzishskij Aleksandr Isaakovich
  • Nesterov Oleg Valeryanovich
RU2624268C1
METHOD OF DETERMINING DEFORMATIONS OF PILE SUPPORTS OF PIPELINE USING NAVIGATION SATELLITE SYSTEMS 2023
  • Elizarov Andrei Sergeevich
RU2821670C1

RU 2 633 093 C1

Authors

Kulikov Dmitrij Anatolevich

Kotov Sergej Nikolaevich

Dates

2017-10-11Published

2016-09-15Filed