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2 338 160

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IPC

G01C23/00(2006-01-01)

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Application

2007123823/28, 2007-06-25

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Start date

2007-06-25

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Actual filing date

2007-06-25

(45)

Published

2008-11-10

(72)

Inventor

Bogdanov Maksim BorisovichSavel'Ev Valerij ViktorovichSmirnov Vladimir AleksandrovichSukhinin Boris VladimirovichProkhortsov Aleksej VjacheslavovichChepurin Aleksandr Aleksandrovich

(73)

Holder

Gosudarstvennoe Obrazovatel'Noe Uchrezhdenie Vysshego Professional'Nogo Obrazovanija Tul'Skij Gosudarstvennyj Universitet

METHOD FOR NAVIGATION PARAMETRE DEFINITION Russian patent published in 2008 - IPC G01C23/00

Abstract RU 2338160 C1

FIELD: physics, measurement.

SUBSTANCE: objective is achieved by combination of satellite and inertial navigation system signals. Corrected navigation parametres and inertial navigation system error values are defined. Error magnitude is transmitted to inertial navigation system to correct navigation parametres produced in the following time moments. Combination is based on data from one navigation satellite. Corrected navigation parametres are defined, and difference between current navigation parametres produced by inertial navigation system and corrected navigation parametre values is used as inertial navigation system error.

EFFECT: extended functional capacities of navigation parametre defining method.

2 dwg

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RU 2 338 160 C1

Authors

Bogdanov Maksim Borisovich

Savel'Ev Valerij Viktorovich

Smirnov Vladimir Aleksandrovich

Sukhinin Boris Vladimirovich

Prokhortsov Aleksej Vjacheslavovich

Chepurin Aleksandr Aleksandrovich

Dates

2008-11-10—Published

2007-06-25—Filed