RU2010123777A - METHOD OF SATELLITE CORRECTION OF AUTONOMOUS MEANS OF NAVIGATION OF MOBILE OBJECTS - Google Patents

METHOD OF SATELLITE CORRECTION OF AUTONOMOUS MEANS OF NAVIGATION OF MOBILE OBJECTS Download PDF

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Publication number
RU2010123777A
RU2010123777A RU2010123777/28A RU2010123777A RU2010123777A RU 2010123777 A RU2010123777 A RU 2010123777A RU 2010123777/28 A RU2010123777/28 A RU 2010123777/28A RU 2010123777 A RU2010123777 A RU 2010123777A RU 2010123777 A RU2010123777 A RU 2010123777A
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Russia
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navigation
satellite
autonomous
correction
autonomous means
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RU2010123777/28A
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Russian (ru)
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RU2448326C2 (en
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Владимир Валентинович Гаврилов (RU)
Владимир Валентинович Гаврилов
Сергей Борисович Курсин (RU)
Сергей Борисович Курсин
Валентина Ивановна Лапшина (RU)
Валентина Ивановна Лапшина
Павел Иванович Малеев (RU)
Павел Иванович Малеев
Original Assignee
ОАО "Государственный научно-исследовательский навигационно-гидрографический институт" (ГНИНГИ) (RU)
ОАО "Государственный научно-исследовательский навигационно-гидрографический институт" (ГНИНГИ)
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Priority to RU2010123777/28A priority Critical patent/RU2448326C2/en
Publication of RU2010123777A publication Critical patent/RU2010123777A/en
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Abstract

Способ спутниковой коррекции автономных средств навигации подвижных объектов, включающий автономные средства измерения местоположения, скорости и курса объекта и приемник спутниковой навигационной системы, отличающийся тем, что выработка спутниковой системой навигационных параметров коррекции базируется на измерениях дальности от объекта до навигационных спутников в три близкие (около 1 с) момента времени и число используемых для этого спутников может быть значительно меньше (в том числе и один), чем при использовании традиционного способа. A method for satellite correction of autonomous navigation tools for moving objects, including autonomous means for measuring the location, speed and course of an object and a satellite navigation system receiver, characterized in that the satellite system produces navigation correction parameters based on measurements of the distance from the object to the navigation satellites in three close ones (about 1 c) the time instant and the number of satellites used for this can be significantly less (including one) than when using the traditional benefits.

Claims (1)

Способ спутниковой коррекции автономных средств навигации подвижных объектов, включающий автономные средства измерения местоположения, скорости и курса объекта и приемник спутниковой навигационной системы, отличающийся тем, что выработка спутниковой системой навигационных параметров коррекции базируется на измерениях дальности от объекта до навигационных спутников в три близкие (около 1 с) момента времени и число используемых для этого спутников может быть значительно меньше (в том числе и один), чем при использовании традиционного способа. A method for satellite correction of autonomous navigation tools for moving objects, including autonomous means for measuring the location, speed and course of an object and a satellite navigation system receiver, characterized in that the satellite system produces navigation correction parameters based on measurements of the distance from the object to the navigation satellites in three close ones (about 1 c) the time instant and the number of satellites used for this can be significantly less (including one) than when using the traditional benefits.
RU2010123777/28A 2010-06-10 2010-06-10 Method for satellite correction of self-contained navigation apparatus of mobile objects RU2448326C2 (en)

Priority Applications (1)

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RU2010123777/28A RU2448326C2 (en) 2010-06-10 2010-06-10 Method for satellite correction of self-contained navigation apparatus of mobile objects

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Application Number Priority Date Filing Date Title
RU2010123777/28A RU2448326C2 (en) 2010-06-10 2010-06-10 Method for satellite correction of self-contained navigation apparatus of mobile objects

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RU2010123777A true RU2010123777A (en) 2011-12-20
RU2448326C2 RU2448326C2 (en) 2012-04-20

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Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2488078C2 (en) * 2011-04-13 2013-07-20 Федеральное государственное унитарное предприятие "Центр эксплуатации объектов наземной космической инфраструктуры" Method and device of gyro instrument positioning in space during its testing
RU2506542C1 (en) * 2012-09-21 2014-02-10 Павел Григорьевич Бродский Method of satellite correction of autonomous facilities of navigation of movable objects

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5570097A (en) * 1995-08-11 1996-10-29 Northrop Grumman Corporation Retransmitted GPS interferometric system
US6107959A (en) * 1996-09-30 2000-08-22 Qualcomm Incorporated Positioning determination using one low-Earth orbit satellite
US7432853B2 (en) * 2003-10-28 2008-10-07 Trimble Navigation Limited Ambiguity estimation of GNSS signals for three or more carriers
RU2308681C1 (en) * 2006-03-22 2007-10-20 Открытое акционерное общество "Специальное конструкторское бюро приборостроения и автоматики" Gyroscopic navigation system for movable objects

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Effective date: 20120611