Single‐step geolocation for a non‐circular source in the presence of satellite orbit perturbations
Abstract This study addresses the problem of geolocating a strictly non‐circular source on the surface of Earth by a cluster of passive satellites. The known satellite positions and velocities are subject to random errors. The authors propose a single‐step satellite geolocation algorithm that direct...
| Main Authors: | , , , |
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| Format: | Article |
| Language: | English |
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Wiley
2022-04-01
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| Series: | IET Signal Processing |
| Subjects: | |
| Online Access: | https://doi.org/10.1049/sil2.12083 |
| _version_ | 1826831860596998144 |
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| author | Jiexin Yin Ding Wang Fuquan Nie Nae Zheng |
| author_facet | Jiexin Yin Ding Wang Fuquan Nie Nae Zheng |
| author_sort | Jiexin Yin |
| collection | DOAJ |
| description | Abstract This study addresses the problem of geolocating a strictly non‐circular source on the surface of Earth by a cluster of passive satellites. The known satellite positions and velocities are subject to random errors. The authors propose a single‐step satellite geolocation algorithm that directly localises the transmitter from sensor outputs using the information of time delays and Doppler shifts but without explicitly estimating them. It exploits the non‐circular property of signals and a priori information of satellite orbit error distribution to jointly calibrate orbit errors and determine the longitude and latitude of the transmitter based on the ellipsoidal Earth model, which integrates an alternating iteration scheme for the estimation of various unknowns instead of the exhaustive grid search. Additionally, a detailed Cramér‐Rao bound (CRB) derivation is presented for the single‐step satellite geolocation of a non‐circular source on Earth with and without satellite orbit perturbations, and it is proved that these CRBs are lower than the associated CRBs for a circular source. The simulation results illustrate that the proposed method asymptotically attains the associated CRB, and shows greater performance robustness to signal‐to‐noise ratio (SNR) and satellite orbit errors compared with conventional two‐step satellite geolocation approaches. |
| first_indexed | 2024-03-09T08:29:43Z |
| format | Article |
| id | doaj.art-5ecc8c981a1a43ddaac179711eeee587 |
| institution | Directory Open Access Journal |
| issn | 1751-9675 1751-9683 |
| language | English |
| last_indexed | 2025-02-16T10:08:10Z |
| publishDate | 2022-04-01 |
| publisher | Wiley |
| record_format | Article |
| series | IET Signal Processing |
| spelling | doaj.art-5ecc8c981a1a43ddaac179711eeee5872025-02-03T01:29:36ZengWileyIET Signal Processing1751-96751751-96832022-04-0116217020010.1049/sil2.12083Single‐step geolocation for a non‐circular source in the presence of satellite orbit perturbationsJiexin Yin0Ding Wang1Fuquan Nie2Nae Zheng3PLA Strategic Support Force Information Engineering University Zhengzhou Henan ChinaPLA Strategic Support Force Information Engineering University Zhengzhou Henan ChinaWeihua Group Co., Ltd Changyuan Henan ChinaPLA Strategic Support Force Information Engineering University Zhengzhou Henan ChinaAbstract This study addresses the problem of geolocating a strictly non‐circular source on the surface of Earth by a cluster of passive satellites. The known satellite positions and velocities are subject to random errors. The authors propose a single‐step satellite geolocation algorithm that directly localises the transmitter from sensor outputs using the information of time delays and Doppler shifts but without explicitly estimating them. It exploits the non‐circular property of signals and a priori information of satellite orbit error distribution to jointly calibrate orbit errors and determine the longitude and latitude of the transmitter based on the ellipsoidal Earth model, which integrates an alternating iteration scheme for the estimation of various unknowns instead of the exhaustive grid search. Additionally, a detailed Cramér‐Rao bound (CRB) derivation is presented for the single‐step satellite geolocation of a non‐circular source on Earth with and without satellite orbit perturbations, and it is proved that these CRBs are lower than the associated CRBs for a circular source. The simulation results illustrate that the proposed method asymptotically attains the associated CRB, and shows greater performance robustness to signal‐to‐noise ratio (SNR) and satellite orbit errors compared with conventional two‐step satellite geolocation approaches.https://doi.org/10.1049/sil2.12083alternating iterationCramér‐Rao bound (CRB)non‐circular signalsatellite geolocationsingle‐step geolocation |
| spellingShingle | Jiexin Yin Ding Wang Fuquan Nie Nae Zheng Single‐step geolocation for a non‐circular source in the presence of satellite orbit perturbations IET Signal Processing alternating iteration Cramér‐Rao bound (CRB) non‐circular signal satellite geolocation single‐step geolocation |
| title | Single‐step geolocation for a non‐circular source in the presence of satellite orbit perturbations |
| title_full | Single‐step geolocation for a non‐circular source in the presence of satellite orbit perturbations |
| title_fullStr | Single‐step geolocation for a non‐circular source in the presence of satellite orbit perturbations |
| title_full_unstemmed | Single‐step geolocation for a non‐circular source in the presence of satellite orbit perturbations |
| title_short | Single‐step geolocation for a non‐circular source in the presence of satellite orbit perturbations |
| title_sort | single step geolocation for a non circular source in the presence of satellite orbit perturbations |
| topic | alternating iteration Cramér‐Rao bound (CRB) non‐circular signal satellite geolocation single‐step geolocation |
| url | https://doi.org/10.1049/sil2.12083 |
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