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Abstract

Emitter localization offers significant advantages such as high concealment, long detection range, and low cost, making it indispensable in target positioning. The utilization of low earth orbit satellite formation with AOA (Angle of Arrival) and TDOA (Time Difference of Arrival) measurements is a key technology for achieving emitter localization. To address the issues of requiring numerous cooperative platforms and the poor accuracy of single-epoch solutions with single-parameter closed-form algorithms, this paper proposes a multi-parameter multi-epoch positioning method based on a three-satellite formation. Simulation data are used to analyze the positioning accuracy under various epochs and different TDOA and AOA noise conditions. The experimental results demonstrate that, compared to the traditional single-parameter single-epoch localization method, utilizing a three-satellite formation with combined AOA and TDOA parameters, along with a multi-epoch solution approach, significantly improves localization accuracy to within an order of ten meters. This method enhances robustness and provides a viable strategy for addressing localization challenges caused by underdetermined systems of equations. Additionally, the results verify that an accumulated almanac element duration of 20 s ensures high positioning accuracy while maintaining a low computational cost. The combined multi-parameter multi-epoch method shows substantial advantages in improving both accuracy and robustness, providing valuable insights for future satellite-based emitter localization technologies.

Details

1009240
Title
Precision Analysis of Multi-Parameter Multi-Epoch Emitter Localization Radar in Three-Satellite Formation
Author
Lian, Yiming 1 ; Wu, Yuxuan 2   VIAFID ORCID Logo  ; Chen, Yaowen 3   VIAFID ORCID Logo  ; Liu, Xian 3   VIAFID ORCID Logo  ; Jiang, Liming 1 

 State Key Laboratory of Geodesy and Earth’s Dynamics, Innovation Academy for Precision Measurement Science and Technology, Chinese Academy of Sciences, Wuhan 430077, China; [email protected] (Y.L.); [email protected] (Y.W.); [email protected] (Y.C.); [email protected] (X.L.); University of Chinese Academy of Sciences, Beijing 100049, China 
 State Key Laboratory of Geodesy and Earth’s Dynamics, Innovation Academy for Precision Measurement Science and Technology, Chinese Academy of Sciences, Wuhan 430077, China; [email protected] (Y.L.); [email protected] (Y.W.); [email protected] (Y.C.); [email protected] (X.L.) 
 State Key Laboratory of Geodesy and Earth’s Dynamics, Innovation Academy for Precision Measurement Science and Technology, Chinese Academy of Sciences, Wuhan 430077, China; [email protected] (Y.L.); [email protected] (Y.W.); [email protected] (Y.C.); [email protected] (X.L.); College of Earth and Planet Science, Chengdu University of Technology, Chengdu 610059, China 
Publication title
Volume
17
Issue
1
First page
96
Publication year
2025
Publication date
2025
Publisher
MDPI AG
Place of publication
Basel
Country of publication
Switzerland
Publication subject
e-ISSN
20724292
Source type
Scholarly Journal
Language of publication
English
Document type
Journal Article
Publication history
 
 
Online publication date
2024-12-30
Milestone dates
2024-10-09 (Received); 2024-12-04 (Accepted)
Publication history
 
 
   First posting date
30 Dec 2024
ProQuest document ID
3153685556
Document URL
https://www.proquest.com/scholarly-journals/precision-analysis-multi-parameter-epoch-emitter/docview/3153685556/se-2?accountid=208611
Copyright
© 2024 by the authors. Licensee MDPI, Basel, Switzerland. This article is an open access article distributed under the terms and conditions of the Creative Commons Attribution (CC BY) license (https://creativecommons.org/licenses/by/4.0/). Notwithstanding the ProQuest Terms and Conditions, you may use this content in accordance with the terms of the License.
Last updated
2025-01-10
Database
ProQuest One Academic