Dachen Peng , Shibo Guo , Defeng Gu , Kai Shao , Houzhe Zhang , Ruiyun Yang , Jufeng Lu , Jiangkai Liu , Haoseng Wang , LiuPeng Huang
{"title":"具有模糊分辨率约束的四星InSAR星座HT-01的精确基线确定","authors":"Dachen Peng , Shibo Guo , Defeng Gu , Kai Shao , Houzhe Zhang , Ruiyun Yang , Jufeng Lu , Jiangkai Liu , Haoseng Wang , LiuPeng Huang","doi":"10.1016/j.asr.2025.03.039","DOIUrl":null,"url":null,"abstract":"<div><div>Distributed interferometric SAR (InSAR) systems is evolving from dual-satellite configurations to multi-satellite systems. The Hongtu-01 constellation (HT-01), world’s first four-satellite interferometric SAR system utilizing a cartwheel formation, marks a significant milestone in China. Precision orbit determination (POD) and precision baseline determination (PBD) are essential for the successful execution of the HT-01 mission. However, baseline determination poses a challenge to differential GPS techniques due to the requirement for simultaneous determination of multiple baselines efficiently. As an alternative, absolute orbit can be computed individually for each spacecraft and used for the generation of precise baseline products. In addition, single-receiver ambiguity resolution (SR-AR) and double-differential ambiguity resolution (DD-AR) could be employed as constraint to enhance the accuracy of POD. In this paper, the performance of orbit and baseline determination for HT-01 is comprehensively evaluated. For further improving POD precision, receiver GPS signal phase center variations (PCV) models with 3 × 3°grid map and maneuver handling was employed. Among POD solutions, the results for the SLR residuals are 2.12 cm, 1.94 cm, 1.59 cm and 1.53 cm corresponding to the ambiguity-float, ambiguity-float + PCV, ambiguity-fixed and ambiguity-fixed + PCV orbit solution, respectively. Furthermore, we analyze the baseline difference between the baseline solution of SR-AR with approximately 92 % ambiguity fixing rates and baseline solution of DD-AR with almost 100 % ambiguity fixing rates. Result exhibit baseline consistency of approximately 1∼2 mm on each direction. Besides, baseline overlapping with 3D RMS consistency shows 1.07 mm and 1.23 mm for DD-AR and SR-AR, respectively. The above solutions can be considered as an effective approach for prospective formation-flying remote sensing missions with multi-baseline determination for a multi-satellite constellation.</div></div>","PeriodicalId":50850,"journal":{"name":"Advances in Space Research","volume":"75 11","pages":"Pages 7917-7931"},"PeriodicalIF":2.8000,"publicationDate":"2025-03-19","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Precise baseline determination for the four-satellite InSAR constellation HT-01 with ambiguity resolution constraints\",\"authors\":\"Dachen Peng , Shibo Guo , Defeng Gu , Kai Shao , Houzhe Zhang , Ruiyun Yang , Jufeng Lu , Jiangkai Liu , Haoseng Wang , LiuPeng Huang\",\"doi\":\"10.1016/j.asr.2025.03.039\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"<div><div>Distributed interferometric SAR (InSAR) systems is evolving from dual-satellite configurations to multi-satellite systems. The Hongtu-01 constellation (HT-01), world’s first four-satellite interferometric SAR system utilizing a cartwheel formation, marks a significant milestone in China. Precision orbit determination (POD) and precision baseline determination (PBD) are essential for the successful execution of the HT-01 mission. However, baseline determination poses a challenge to differential GPS techniques due to the requirement for simultaneous determination of multiple baselines efficiently. As an alternative, absolute orbit can be computed individually for each spacecraft and used for the generation of precise baseline products. In addition, single-receiver ambiguity resolution (SR-AR) and double-differential ambiguity resolution (DD-AR) could be employed as constraint to enhance the accuracy of POD. In this paper, the performance of orbit and baseline determination for HT-01 is comprehensively evaluated. For further improving POD precision, receiver GPS signal phase center variations (PCV) models with 3 × 3°grid map and maneuver handling was employed. Among POD solutions, the results for the SLR residuals are 2.12 cm, 1.94 cm, 1.59 cm and 1.53 cm corresponding to the ambiguity-float, ambiguity-float + PCV, ambiguity-fixed and ambiguity-fixed + PCV orbit solution, respectively. Furthermore, we analyze the baseline difference between the baseline solution of SR-AR with approximately 92 % ambiguity fixing rates and baseline solution of DD-AR with almost 100 % ambiguity fixing rates. Result exhibit baseline consistency of approximately 1∼2 mm on each direction. Besides, baseline overlapping with 3D RMS consistency shows 1.07 mm and 1.23 mm for DD-AR and SR-AR, respectively. The above solutions can be considered as an effective approach for prospective formation-flying remote sensing missions with multi-baseline determination for a multi-satellite constellation.</div></div>\",\"PeriodicalId\":50850,\"journal\":{\"name\":\"Advances in Space Research\",\"volume\":\"75 11\",\"pages\":\"Pages 7917-7931\"},\"PeriodicalIF\":2.8000,\"publicationDate\":\"2025-03-19\",\"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/S0273117725002571\",\"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}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"Advances in Space Research","FirstCategoryId":"89","ListUrlMain":"https://www.sciencedirect.com/science/article/pii/S0273117725002571","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}
Precise baseline determination for the four-satellite InSAR constellation HT-01 with ambiguity resolution constraints
Distributed interferometric SAR (InSAR) systems is evolving from dual-satellite configurations to multi-satellite systems. The Hongtu-01 constellation (HT-01), world’s first four-satellite interferometric SAR system utilizing a cartwheel formation, marks a significant milestone in China. Precision orbit determination (POD) and precision baseline determination (PBD) are essential for the successful execution of the HT-01 mission. However, baseline determination poses a challenge to differential GPS techniques due to the requirement for simultaneous determination of multiple baselines efficiently. As an alternative, absolute orbit can be computed individually for each spacecraft and used for the generation of precise baseline products. In addition, single-receiver ambiguity resolution (SR-AR) and double-differential ambiguity resolution (DD-AR) could be employed as constraint to enhance the accuracy of POD. In this paper, the performance of orbit and baseline determination for HT-01 is comprehensively evaluated. For further improving POD precision, receiver GPS signal phase center variations (PCV) models with 3 × 3°grid map and maneuver handling was employed. Among POD solutions, the results for the SLR residuals are 2.12 cm, 1.94 cm, 1.59 cm and 1.53 cm corresponding to the ambiguity-float, ambiguity-float + PCV, ambiguity-fixed and ambiguity-fixed + PCV orbit solution, respectively. Furthermore, we analyze the baseline difference between the baseline solution of SR-AR with approximately 92 % ambiguity fixing rates and baseline solution of DD-AR with almost 100 % ambiguity fixing rates. Result exhibit baseline consistency of approximately 1∼2 mm on each direction. Besides, baseline overlapping with 3D RMS consistency shows 1.07 mm and 1.23 mm for DD-AR and SR-AR, respectively. The above solutions can be considered as an effective approach for prospective formation-flying remote sensing missions with multi-baseline determination for a multi-satellite constellation.
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.