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Design and Algorithm Verification of Precision Navigation System

Authors :
Sanguk Lee
Tae-Hee Kim
Seongkyun Jeong
Jae-Eun Lee
Source :
Journal of the Korean Society for Aviation and Aeronautics. 21:8-14
Publication Year :
2013
Publisher :
The Korean Society for Aviation and Aeronautics, 2013.

Abstract

As GNSS(Global Navigation Satellite System) is used in various filed, many countries establish GNSS system independently. But GNSS system has the limitation of accuracy and stability in stand-alone mode, because this system has error elements which are ionospheric delay, tropospheric delay, orbit ephemeris error, satellite clock error, and etc. For overcome of accuracy limitation, the DGPS(Differential GPS) and RTK(Real-Time Kinematic) systems are proposed. These systems perform relative positioning using the reference and user receivers. ETRI(Electronics and Telecommunications Research Institute) is developing precision navigation system in point of extension of GNSS usage. The precision navigation system is for providing the precision navigation solution to common users. If this technology is developed, GNSS system can be used in the fields which require precision positioning and control. In this paper, we introduce the precision navigation system and perform design and algorithm verification.

Details

ISSN :
12259705
Volume :
21
Database :
OpenAIRE
Journal :
Journal of the Korean Society for Aviation and Aeronautics
Accession number :
edsair.doi...........99cf9da6bda32a0f56c84c5c9385ca6e
Full Text :
https://doi.org/10.12985/ksaa.2013.21.1.008