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2 329 469

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(51)

IPC

G01C23/00(2006-01-01)

(21) (22)

Application

2007109919/28, 2007-03-19

(24)

Start date

2007-03-19

(22)

Actual filing date

2007-03-19

(45)

Published

2008-07-20

(72)

Inventor

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

(73)

Holder

Tul'Skij Gosudarstvennyj Universitet

METHOD OF DEFINITION OF NAVIGATION PARAMETERS Russian patent published in 2008 - IPC G01C23/00

Abstract RU 2329469 C1

FIELD: instrument making.

SUBSTANCE: invention can be used in designing the integrated navigation systems, in particular, for objects with minor operating period. To this end, the inertial and satellite navigation systems signals are gathered and processed. Here, integration of measurement errors is effected using the signals from two navigation satellites proceeding from the primary radio navigation parameters generated by the satellite navigation system receivers hardware. The corrected parameters of navigation are defined, and the difference between current parameters of navigation are taken for sizes of errors of the inertial navigating system.

EFFECT: expanded potentialities.

2 dwg

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RU 2 329 469 C1

Authors

Bogdanov Maksim Borisovich

Savel'Ev Valerij Viktorovich

Smirnov Vladimir Aleksandrovich

Sukhinin Boris Vladimirovich

Prokhortsov Aleksej Vjacheslavovich

Chepurin Aleksandr Aleksandrovich

Dates

2008-07-20—Published

2007-03-19—Filed