Precision Analysis of Multi-Parameter Multi-Epoch Emitter Localization Radar in Three-Satellite Formation

Uloženo v:
Podrobná bibliografie
Vydáno v:Remote Sensing vol. 17, no. 1 (2025), p. 96
Hlavní autor: Lian, Yiming
Další autoři: Wu, Yuxuan, Chen, Yaowen, Liu, Xian, Jiang, Liming
Vydáno:
MDPI AG
Témata:
On-line přístup:Citation/Abstract
Full Text + Graphics
Full Text - PDF
Tagy: Přidat tag
Žádné tagy, Buďte první, kdo vytvoří štítek k tomuto záznamu!

MARC

LEADER 00000nab a2200000uu 4500
001 3153685556
003 UK-CbPIL
022 |a 2072-4292 
024 7 |a 10.3390/rs17010096  |2 doi 
035 |a 3153685556 
045 2 |b d20250101  |b d20251231 
084 |a 231556  |2 nlm 
100 1 |a Lian, Yiming  |u 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>lianyiming23@mails.ucas.ac.cn</email> (Y.L.); <email>wuyuxuan@apm.ac.cn</email> (Y.W.); <email>chenyaowen@stu.cdut.edu.cn</email> (Y.C.); <email>liuxian@stu.cdut.edu.cn</email> (X.L.); University of Chinese Academy of Sciences, Beijing 100049, China 
245 1 |a Precision Analysis of Multi-Parameter Multi-Epoch Emitter Localization Radar in Three-Satellite Formation 
260 |b MDPI AG  |c 2025 
513 |a Journal Article 
520 3 |a 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. 
653 |a Radio communications 
653 |a Accuracy 
653 |a Localization method 
653 |a Radar detection 
653 |a Measuring instruments 
653 |a Angle of arrival 
653 |a Sensors 
653 |a Target detection 
653 |a Computing costs 
653 |a Parameter robustness 
653 |a Algorithms 
653 |a Satellites 
653 |a Methods 
653 |a Spectrum allocation 
653 |a Localization 
653 |a Robustness (mathematics) 
653 |a Earth orbits 
653 |a Low earth orbits 
653 |a Radiation 
653 |a Linear equations 
653 |a Emitters 
700 1 |a Wu, Yuxuan  |u 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>lianyiming23@mails.ucas.ac.cn</email> (Y.L.); <email>wuyuxuan@apm.ac.cn</email> (Y.W.); <email>chenyaowen@stu.cdut.edu.cn</email> (Y.C.); <email>liuxian@stu.cdut.edu.cn</email> (X.L.) 
700 1 |a Chen, Yaowen  |u 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>lianyiming23@mails.ucas.ac.cn</email> (Y.L.); <email>wuyuxuan@apm.ac.cn</email> (Y.W.); <email>chenyaowen@stu.cdut.edu.cn</email> (Y.C.); <email>liuxian@stu.cdut.edu.cn</email> (X.L.); College of Earth and Planet Science, Chengdu University of Technology, Chengdu 610059, China 
700 1 |a Liu, Xian  |u 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>lianyiming23@mails.ucas.ac.cn</email> (Y.L.); <email>wuyuxuan@apm.ac.cn</email> (Y.W.); <email>chenyaowen@stu.cdut.edu.cn</email> (Y.C.); <email>liuxian@stu.cdut.edu.cn</email> (X.L.); College of Earth and Planet Science, Chengdu University of Technology, Chengdu 610059, China 
700 1 |a Jiang, Liming  |u 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>lianyiming23@mails.ucas.ac.cn</email> (Y.L.); <email>wuyuxuan@apm.ac.cn</email> (Y.W.); <email>chenyaowen@stu.cdut.edu.cn</email> (Y.C.); <email>liuxian@stu.cdut.edu.cn</email> (X.L.); University of Chinese Academy of Sciences, Beijing 100049, China 
773 0 |t Remote Sensing  |g vol. 17, no. 1 (2025), p. 96 
786 0 |d ProQuest  |t Advanced Technologies & Aerospace Database 
856 4 1 |3 Citation/Abstract  |u https://www.proquest.com/docview/3153685556/abstract/embedded/L8HZQI7Z43R0LA5T?source=fedsrch 
856 4 0 |3 Full Text + Graphics  |u https://www.proquest.com/docview/3153685556/fulltextwithgraphics/embedded/L8HZQI7Z43R0LA5T?source=fedsrch 
856 4 0 |3 Full Text - PDF  |u https://www.proquest.com/docview/3153685556/fulltextPDF/embedded/L8HZQI7Z43R0LA5T?source=fedsrch