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 PDFInfo
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- 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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- navigation
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- autonomous
- correction
- autonomous means
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- Position Fixing By Use Of Radio Waves (AREA)
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.
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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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RU2010123777/28A RU2448326C2 (en) | 2010-06-10 | 2010-06-10 | Method for satellite correction of self-contained navigation apparatus of mobile objects |
Publications (2)
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RU2010123777A true RU2010123777A (en) | 2011-12-20 |
RU2448326C2 RU2448326C2 (en) | 2012-04-20 |
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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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Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
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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)
Publication number | Priority date | Publication date | Assignee | Title |
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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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RU2448326C2 (en) | 2012-04-20 |
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MM4A | The patent is invalid due to non-payment of fees |
Effective date: 20120611 |