{"title":"Orbit determination analysis of IGSO satellite onboard GPS/BDS pseudorange data corrected by different code hardware delays products","authors":"Zhenghao Zhang , Yong Huang , Peng Yang , Yanling Chen , Xiaolin Jia","doi":"10.1016/j.asr.2024.11.047","DOIUrl":null,"url":null,"abstract":"<div><div>The navigation signal received by the Inclined Geo-Synchronous Orbit (IGSO) satellite is often blocked by the Earth, and the signal strength is weak due to the long propagation distance, which makes the carrier phase data processing complicated. Using pseudorange data is a convenient and efficient method for determining the orbit of IGSO satellites. Code hardware delays are non-negligible errors in pseudorange data processing. This study investigates the precise orbit determination (POD) result using only pseudorange data corrected by four types of Differential Code Bias (DCB) products and Observable-specific Signal Biases (OSB) products, with the LT4A satellite as a case study. The results show that the correction of code hardware delay can effectively improve the orbit quality. After correcting the code hardware delay, using only GPS pseudorange observations, using only BDS pseudorange observations, and using GPS + BDS combined pseudorange observations to determine the orbit, the pseudorange residuals RMS are about 1.82 m, 1.09 m, and 1.53 m, respectively. Compared with the uncorrected code hardware delays results, the residuals RMS is better by 21.8 %, 79.5 %, and 53.0 %, respectively. As the length of the POD arc increases from 24 h to 72 h, both the quality and stability of the orbit are observed to improve. For the 72 h arc, the orbit overlap RMS with the three data types is 3.4 m, 3.0 m, and 2.8 m, respectively, with the improvement of about 10.5 %, 77.6 %, and 59.4 %, respectively, compared with no code hardware delays correction. Compared with the precise reference orbit, the comparison RMS are 6.3 m, 4.8 m, and 4.4 m, increased by 24.0 %, 78.9 %, and 51.6 %, respectively. The results demonstrate that the comparison RMS of the IGSO satellite with only pseudorange data can be better than 5 m in position, and correcting the code hardware delays can improve orbit quality obviously, especially for BDS pseudorange data.</div></div>","PeriodicalId":50850,"journal":{"name":"Advances in Space Research","volume":"75 3","pages":"Pages 3050-3062"},"PeriodicalIF":2.8000,"publicationDate":"2025-02-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"Advances in Space Research","FirstCategoryId":"89","ListUrlMain":"https://www.sciencedirect.com/science/article/pii/S0273117724011694","RegionNum":3,"RegionCategory":"地球科学","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q2","JCRName":"ASTRONOMY & ASTROPHYSICS","Score":null,"Total":0}
引用次数: 0
Abstract
The navigation signal received by the Inclined Geo-Synchronous Orbit (IGSO) satellite is often blocked by the Earth, and the signal strength is weak due to the long propagation distance, which makes the carrier phase data processing complicated. Using pseudorange data is a convenient and efficient method for determining the orbit of IGSO satellites. Code hardware delays are non-negligible errors in pseudorange data processing. This study investigates the precise orbit determination (POD) result using only pseudorange data corrected by four types of Differential Code Bias (DCB) products and Observable-specific Signal Biases (OSB) products, with the LT4A satellite as a case study. The results show that the correction of code hardware delay can effectively improve the orbit quality. After correcting the code hardware delay, using only GPS pseudorange observations, using only BDS pseudorange observations, and using GPS + BDS combined pseudorange observations to determine the orbit, the pseudorange residuals RMS are about 1.82 m, 1.09 m, and 1.53 m, respectively. Compared with the uncorrected code hardware delays results, the residuals RMS is better by 21.8 %, 79.5 %, and 53.0 %, respectively. As the length of the POD arc increases from 24 h to 72 h, both the quality and stability of the orbit are observed to improve. For the 72 h arc, the orbit overlap RMS with the three data types is 3.4 m, 3.0 m, and 2.8 m, respectively, with the improvement of about 10.5 %, 77.6 %, and 59.4 %, respectively, compared with no code hardware delays correction. Compared with the precise reference orbit, the comparison RMS are 6.3 m, 4.8 m, and 4.4 m, increased by 24.0 %, 78.9 %, and 51.6 %, respectively. The results demonstrate that the comparison RMS of the IGSO satellite with only pseudorange data can be better than 5 m in position, and correcting the code hardware delays can improve orbit quality obviously, especially for BDS pseudorange data.
期刊介绍:
The COSPAR publication Advances in Space Research (ASR) is an open journal covering all areas of space research including: space studies of the Earth''s surface, meteorology, climate, the Earth-Moon system, planets and small bodies of the solar system, upper atmospheres, ionospheres and magnetospheres of the Earth and planets including reference atmospheres, space plasmas in the solar system, astrophysics from space, materials sciences in space, fundamental physics in space, space debris, space weather, Earth observations of space phenomena, etc.
NB: Please note that manuscripts related to life sciences as related to space are no more accepted for submission to Advances in Space Research. Such manuscripts should now be submitted to the new COSPAR Journal Life Sciences in Space Research (LSSR).
All submissions are reviewed by two scientists in the field. COSPAR is an interdisciplinary scientific organization concerned with the progress of space research on an international scale. Operating under the rules of ICSU, COSPAR ignores political considerations and considers all questions solely from the scientific viewpoint.