Use spatial information in integrated inertial-satellite navigation systems of aircraft
Abstract
The tightly coupled integration with serial measurement processing of the pseudo ranges and carrier Doppler measurements is investigated. The spatial information of inertial navigation systems is used for determination satellite attitude relative to directional diagram and for signal search stoppage at the time of the flight maneuver.
About the Authors
A. I. Sokolov
Saint Petersburg Electrotechnical University "LETI"
Russian Federation
Russian Federation
Y. S. Yurchenko
Saint Petersburg Electrotechnical University "LETI"
Russian Federation
Russian Federation
References
1. ГЛОНАСС. Принципы построения и функционирования / под ред. А. И. Перова, В. Н. Харисова. 3-е изд. М.: Радиотехника, 2005. 688 с.
2. Pat. US 20100106416 A1. Int. Cl. G01C 21/00, G06F 17/00. Aircraft navigation using the global positioning system, inertial reference system and distance measurements / T. E. Yochum. Pub. Date 29.04.2010.
3. Пат. РФ 2536768 C1. МПК G01C 21/00, G01C 23/00. Способ инерциально-спутниковой навигации летательных аппаратов / В. И. Бабуров, А. И. Соколов, Ю. С. Юрченко и др.; опубл. 27.12.2014. Бюл. № 36.
4. Titterton D. H., Weston J. L. Strapdown Inertial Navigation Technology. 2nd ed. Cambridge: MIT Press, 2007. 558 p.
5. Бартон Д. Радиолокационные системы. М.: Воен. изд-во, 1967. 488 c.
6. Радиосистемы управления / В. А. Вейцель, А. С. Волковский, С. А. Волковский и др.; под ред. В. А. Вейцеля. М.: Дрофа, 2005. 416 c.
7. Grewal M. S., Weill L. S., Andrews A. P. Global Positioning Systems, Inertial Navigation, and Integration. 2nd ed. New York: John Wiley & Sons, 2007. 525 p.
Review
For citations:
Sokolov A.I., Yurchenko Y.S. Use spatial information in integrated inertial-satellite navigation systems of aircraft. Journal of the Russian Universities. Radioelectronics. 2015;(5):51-56. (In Russ.)
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