다중 위성 GNSS PPP 정확도 향상을 위한 거리, 고도각 및 SNR 기반 가중값 모델 개발

Development of Weighting Model Considering Range, Elevation Angle, and SNR for Multi-GNSS PPP

초록

Multi- Global Navigation Satellite System (GNSS) integration is widely recognized as an effective approach to improve positioning accuracy and reduce convergence time. However, issues of performance degradation regarding certain satellite constellations have been raised, particularly some BeiDou satellites in Geostationary Earth Orbit (GEO), due to orbit-related errors. To address this, the present study proposes a novel weighting model that maintains the advantages of multi-GNSS integration while minimizing the adverse effects by applying differential weights based on satellite constellation characteristics. The proposed model calculates satellite weights by comprehensively considering satellite-to-receiver range, elevation angle, and signal-to-noise ratio (SNR), and quantitatively reflects the physical characteristics of each constellation—Medium Earth Orbit (MEO), Inclined Geosynchronous Orbit (IGSO), and GEO. Using GNSS data collected over a 12-hour period, this study applies a least-squares-based Precise Point Positioning method using pseudorange measurements with State Space Representation (SSR) corrections. The positioning performance of two weighting strategies is compared: one using elevation and SNR, and the other incorporating range, elevation, and SNR. The results show that the model considering all three factors—range, elevation, and SNR—improved the average positioning accuracy by 3.1%, with a maximum improvement of 9.7%. Additionally, a low standard deviation of 4.1% indicates consistent performance enhancement, and demonstrates the effectiveness of the proposed differential weighting approach.

키워드

다중 위성 항법최소제곱추정코드 의사거리정밀 단독 측위multi-GNSSleast squares estimationcode pseudorangePPP
제목
다중 위성 GNSS PPP 정확도 향상을 위한 거리, 고도각 및 SNR 기반 가중값 모델 개발
제목 (타언어)
Development of Weighting Model Considering Range, Elevation Angle, and SNR for Multi-GNSS PPP
저자
이형석한정민박관동
DOI
10.11003/JPNT.2025.14.2.149
발행일
2025-06
유형
Y
저널명
Journal of Positioning, Navigation, and Timing
14
2
페이지
149 ~ 155