Journal of Advanced Navigation Technology (한국항행학회논문지)

The Korean Navigation Institute (한국항행학회)
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Precise Orbit Estimation of GPS using GIPSY-OASIS

GIPSY-OASIS기반 GPS 정밀 궤도 추정

  • Ha, Jihyun (PP-Solution Corporation) ;
  • Chun, Sebum (Navigation Research and Development Division, Korea Aerospace Research Institute) ;
  • Park, Kwan-Dong (Department of Geoinformatic Engineering, Inha University)
  • 하지현 (주식회사 피피솔) ;
  • 천세범 (한국항공우주연구원 항법기술연구실) ;
  • 박관동 (인하대학교 공간정보공학과)
  • Received : 2019.11.28
  • Accepted : 2019.12.27
  • Published : 2019.12.30
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Abstract

In this paper, scripts for estimating the reference orbits of navigation satellites were developed and their performance was analyzed as a preliminary study for the development of the Korean GPS precise orbit determination technology. The JPL Flinn AC's data processing strategy was applied and Linux-based scripts were developed using GIPSY-OASIS. For the analysis of the accuracy of the estimated reference orbit, the precise orbit provided by the international GNSS data center was used as the truth. As a result, estimated satellite coordinates showed almost exactly same patterns and trends with the reference precise orbits, and their differences are in the range of ±2 cm. The average error between the two orbits was less than 1 cm in the 3D direction, while the standard deviation was also at 1 cm. From these, we found that the developed scripts have excellent performance in precise orbit determination.

이 논문에서는 한국형 GPS 정밀궤도 결정 기술 개발을 위한 기반 연구로써 항법위성의 기준궤도 추정을 위한 스크립트를 개발하고 성능을 분석하였다. 이를 위해 JPL Flinn AC의 자료처리 전략을 적용하였으며, GIPSY-OASIS를 이용하여 리눅스기반 스크립트를 개발하였다. 추정된 기준궤도의 정확도 분석을 위해 국제 데이터센터에서 제공되고 있는 정밀궤도력과 비교하였다. 그 결과 추정된 기준궤도와 정밀궤도력 간 위성좌표가 거의 동일한 경향을 보였으며, 분석 시작 및 종료 시점에서 일부 위성의 오차가 비교적 큰 것으로 나타났으나 대부분의 위성이 ±2 cm 범위에서 수렴하는 것으로 나타났다. 두 궤도력 간 평균오차는 모든 방향으로 1 cm 이하로 나타났으며, 표준편차 역시 1 cm 수준으로 나타나 기준궤도 추정성능이 우수한 것을 알 수 있었다.

Keywords

References

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