Fan Wu , Rui Zou , Zichen Zhao , Xinlong Le , Ruichen Xi
{"title":"DSL 任务中环月卫星编队的相对导航:不完整观测数据的实时解决方案","authors":"Fan Wu , Rui Zou , Zichen Zhao , Xinlong Le , Ruichen Xi","doi":"10.1016/j.ast.2025.110196","DOIUrl":null,"url":null,"abstract":"<div><div>DSL (Discovering the sky at the longest wavelengths) mission is crucial for probing the cosmic dawn and dark ages through ultra-long wavelength observations. However, it presents significant navigation challenges due to GNSS signal loss, difficulty in obtaining relative measurements and severe orbital ambiguity problem. Considering these factors, this paper proposes a cooperative relative navigation strategy for the DSL mission's incomplete inter-satellite observations, consisting of three main parts: unanchored positioning, anchor nodes positioning and coordinate registration. Firstly, we obtain unanchored positions using inter-satellite range information through a multi-satellite cooperative localization method, which can quickly resolve relative positions even with missing range measurements. Secondly, considering the incomplete angle measurements caused by field of view limitations and illumination conditions, we design a new information fusion and complementary method to determine positions of the ANS (Anchor Node Satellites). Thirdly, to achieve high-precision coordinate registration, we propose a covariance-weighted Procrustes analysis algorithm based on positioning accuracies of different anchor nodes to transform unanchored satellite positions into the desired coordinate system. These three proposed algorithms are combined as a fused navigation strategy. Numerical simulations of two practical cases, clustering and trailing formation in the DSL mission, validate the effectiveness of the proposed method, showing the efficiency dealing with incomplete measurement information. Specifically, even with only 30 % angle measurements and 70 % range measurements, the proposed method can still maintain 5-meter accuracy within a distance of 100 km under 50 μrad angle-measuring error and 0.1 m ranging error.</div></div>","PeriodicalId":50955,"journal":{"name":"Aerospace Science and Technology","volume":"162 ","pages":"Article 110196"},"PeriodicalIF":5.0000,"publicationDate":"2025-04-08","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Relative navigation of circumlunar satellite formation in DSL mission: Real-time solution for incomplete observations\",\"authors\":\"Fan Wu , Rui Zou , Zichen Zhao , Xinlong Le , Ruichen Xi\",\"doi\":\"10.1016/j.ast.2025.110196\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"<div><div>DSL (Discovering the sky at the longest wavelengths) mission is crucial for probing the cosmic dawn and dark ages through ultra-long wavelength observations. However, it presents significant navigation challenges due to GNSS signal loss, difficulty in obtaining relative measurements and severe orbital ambiguity problem. Considering these factors, this paper proposes a cooperative relative navigation strategy for the DSL mission's incomplete inter-satellite observations, consisting of three main parts: unanchored positioning, anchor nodes positioning and coordinate registration. Firstly, we obtain unanchored positions using inter-satellite range information through a multi-satellite cooperative localization method, which can quickly resolve relative positions even with missing range measurements. Secondly, considering the incomplete angle measurements caused by field of view limitations and illumination conditions, we design a new information fusion and complementary method to determine positions of the ANS (Anchor Node Satellites). Thirdly, to achieve high-precision coordinate registration, we propose a covariance-weighted Procrustes analysis algorithm based on positioning accuracies of different anchor nodes to transform unanchored satellite positions into the desired coordinate system. These three proposed algorithms are combined as a fused navigation strategy. Numerical simulations of two practical cases, clustering and trailing formation in the DSL mission, validate the effectiveness of the proposed method, showing the efficiency dealing with incomplete measurement information. Specifically, even with only 30 % angle measurements and 70 % range measurements, the proposed method can still maintain 5-meter accuracy within a distance of 100 km under 50 μrad angle-measuring error and 0.1 m ranging error.</div></div>\",\"PeriodicalId\":50955,\"journal\":{\"name\":\"Aerospace Science and Technology\",\"volume\":\"162 \",\"pages\":\"Article 110196\"},\"PeriodicalIF\":5.0000,\"publicationDate\":\"2025-04-08\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"Aerospace Science and Technology\",\"FirstCategoryId\":\"5\",\"ListUrlMain\":\"https://www.sciencedirect.com/science/article/pii/S1270963825002676\",\"RegionNum\":1,\"RegionCategory\":\"工程技术\",\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"Q1\",\"JCRName\":\"ENGINEERING, AEROSPACE\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"Aerospace Science and Technology","FirstCategoryId":"5","ListUrlMain":"https://www.sciencedirect.com/science/article/pii/S1270963825002676","RegionNum":1,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q1","JCRName":"ENGINEERING, AEROSPACE","Score":null,"Total":0}
Relative navigation of circumlunar satellite formation in DSL mission: Real-time solution for incomplete observations
DSL (Discovering the sky at the longest wavelengths) mission is crucial for probing the cosmic dawn and dark ages through ultra-long wavelength observations. However, it presents significant navigation challenges due to GNSS signal loss, difficulty in obtaining relative measurements and severe orbital ambiguity problem. Considering these factors, this paper proposes a cooperative relative navigation strategy for the DSL mission's incomplete inter-satellite observations, consisting of three main parts: unanchored positioning, anchor nodes positioning and coordinate registration. Firstly, we obtain unanchored positions using inter-satellite range information through a multi-satellite cooperative localization method, which can quickly resolve relative positions even with missing range measurements. Secondly, considering the incomplete angle measurements caused by field of view limitations and illumination conditions, we design a new information fusion and complementary method to determine positions of the ANS (Anchor Node Satellites). Thirdly, to achieve high-precision coordinate registration, we propose a covariance-weighted Procrustes analysis algorithm based on positioning accuracies of different anchor nodes to transform unanchored satellite positions into the desired coordinate system. These three proposed algorithms are combined as a fused navigation strategy. Numerical simulations of two practical cases, clustering and trailing formation in the DSL mission, validate the effectiveness of the proposed method, showing the efficiency dealing with incomplete measurement information. Specifically, even with only 30 % angle measurements and 70 % range measurements, the proposed method can still maintain 5-meter accuracy within a distance of 100 km under 50 μrad angle-measuring error and 0.1 m ranging error.
期刊介绍:
Aerospace Science and Technology publishes articles of outstanding scientific quality. Each article is reviewed by two referees. The journal welcomes papers from a wide range of countries. This journal publishes original papers, review articles and short communications related to all fields of aerospace research, fundamental and applied, potential applications of which are clearly related to:
• The design and the manufacture of aircraft, helicopters, missiles, launchers and satellites
• The control of their environment
• The study of various systems they are involved in, as supports or as targets.
Authors are invited to submit papers on new advances in the following topics to aerospace applications:
• Fluid dynamics
• Energetics and propulsion
• Materials and structures
• Flight mechanics
• Navigation, guidance and control
• Acoustics
• Optics
• Electromagnetism and radar
• Signal and image processing
• Information processing
• Data fusion
• Decision aid
• Human behaviour
• Robotics and intelligent systems
• Complex system engineering.
Etc.