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研究生: 吳柏漢
Wu, Bo-Han
論文名稱: 利用全球導航衛星系統反射接收儀之延遲–都卜勒映射資料實現窄帶連續波干擾源定位
Localization of Narrowband CW Interferer Using GNSS-R Delay-Doppler Maps
指導教授: 莊智清
Juang, Jyh-Ching
學位類別: 碩士
Master
系所名稱: 電機資訊學院 - 電機工程學系
Department of Electrical Engineering
論文出版年: 2025
畢業學年度: 113
語文別: 英文
論文頁數: 73
中文關鍵詞: 全球衛星導航系統反射接收儀延遲–都卜勒映射資料射頻干擾定位窄帶連續波干擾都卜勒頻移估計
外文關鍵詞: GNSS-R, Delay-Doppler Map, RF Interference Localization, Narrowband CW Interference, Doppler Shift Estimation
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  • 當全球導航衛星系統 (GNSS) 之頻段受到干擾時,全球導航衛星系統反射接收儀 (GNSS-R) 的延遲–都卜勒映射圖(Delay-Doppler Map)資料的訊雜比顯著下降,使得風速反演等典型任務難以展開。本研究針對此類資料開發全新應用,提出僅基於單一GNSS-R衛星延遲–都卜勒映射資料反推出窄帶單頻或多頻連續波類干擾源位置的方法。首先,針對此類干擾在延遲–都卜勒映射資料上呈現的條紋特徵提取都卜勒頻移,並參考相關文獻方法,利用最小二乘估計(LSE)構建同時包含都卜勒頻移與頻移率的代價函數;隨後於以經緯度–頻偏空間中進行網格搜尋以完成粗定位;最終採用梯度下降演算法,對發射源位置與頻偏參數進行精細定位。為驗證方法可行性,實驗分別以通用軟體無線電平台 (USRP) 產生模擬射頻訊號輸入獵風者衛星同款GNSS-R 接收機產生之延遲–都卜勒映射資料,以及獵風者衛星實際受干擾的延遲–都卜勒映射資料上進行測試。結果顯示,本方法將定位誤差控制在數十公里量級,可應用於干擾發射源的大範圍初步定位,輔助後續精準跟蹤。

    When Global Navigation Satellite System (GNSS) frequency bands are affected by interference, the signal-to-noise ratio (SNR) of Global Navigation Satellite System-Reflectometry (GNSS-R) Delay-Doppler Map (DDM) data drops significantly, hindering conventional applications such as wind speed retrieval. This study proposes a novel use of such data: a method for locating narrowband continuous wave (CW) interference sources, whether single- or multi-frequency—using only DDM data from a single GNSS-R satellite. The approach begins by extracting Doppler shifts from the stripe-like features caused by the interference in DDM. Building on existing methods, a cost function incorporating both Doppler shifts and their rates is formulated using least squares estimation (LSE). A coarse localization is then performed through grid search in the latitude–longitude–frequency shift space, followed by fine-tuning using a gradient descent algorithm to estimate the emitter’s position and frequency parameters. To validate the approach, experiments are conducted using both simulated Radio Frequency (RF) signals generated with a Universal Software Radio Peripheral (USRP) and actual interference-affected DDM data from the TRITON GNSS-R satellite. Results show that the method can constrain the localization error to within tens of kilometers, making it suitable for large-scale preliminary localization of interference transmitters and aiding subsequent precise tracking.

    摘要 II Abstract III 致謝 V Content VI List of Tables IX List of Figures X List of Acronyms XII Chapter 1. Introduction 1 1.1 Research Motivation 1 1.2 Literature Review 1 1.3 Contribution 3 1.4 Thesis Organization 3 Chapter 2. Background 5 2.1 Delay-Doppler Map Data Acquisition 5 2.2 Narrowband CW Interference in DDM 6 2.3 Wideband CW Interference in DDM 8 2.4 Impact of Interference on Signal-to-Noise Ratio (SNR) 10 2.5 IF and DDM Data in GNSS-R 10 Chapter 3. Methodology 12 3.1 Overview 12 3.2 Assumptions 13 3.3 Stripe Feature Extraction 13 3.3.1 Noise-Floor Region Selection 13 3.3.2 Stripe-Array Computation 14 3.4 Stripe Displacement Estimation 15 3.4.1 Sliding-Window Correlation 16 3.4.2 Weighted Fusion Correction 18 3.5 Residual Doppler Shift Estimation 19 3.6 Doppler‐Rate Estimation 22 3.7 Least‐Squares Cost Function 23 3.7.1 Definitions 23 3.7.2 Geometric Characteristics of the Cost Function 24 3.8 Grid Search for Cost-Function Minimization 28 3.9 Fine‐Tuning via Gradient Descent 28 3.9.1 Gradient Equations 29 3.9.2 Adam Optimization Algorithm 30 3.10 Summary 31 Chapter 4. Experiment and Results 33 4.1 Simulated Experiment 33 4.1.1 Environment Setup 33 4.1.2 GNSS-R Satellite Trajectory Generation 35 4.1.3 Zenith-Channel GPS Signal Simulation 36 4.1.4 Nadir-Channel RF Signal Simulation 36 4.1.5 DDM data Specifications 37 4.1.6 Stripe Feature Extraction 38 4.1.7 Grid Search and Gradient Descent Parameters 39 4.1.8 Evaluation of Residual Doppler Shift Tracking 40 4.1.9 Localization Results 46 4.2 Experiment on Real TRITON Satellite DDM 50 4.2.1 Using Packet: Year 2025, Day 061, GPS Second 200621 50 Chapter 5. Conclusions and Future Work 54 5.1 Conclusions 54 5.2 Future Work 55 References 57

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