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研究生: 陳侑炘
Chen, Yu-Hsin
論文名稱: 改良式雙天線整合導航演算法於車載系統應用之研究
Investigation of a Modified Dual-Antenna Integrated Navigation Algorithm and Its Application to Vehicle Systems
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: 2019
畢業學年度: 107
語文別: 英文
論文頁數: 74
中文關鍵詞: 整合導航衛星導航虛擬觀測量雙天線低成本感測器定位效能分析
外文關鍵詞: Navigation, GNSS/INS Integration, Dual-Antenna, Pseudo Measurements, Low-Cost Sensors, Positioning Performance
相關次數: 點閱:73下載:4
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  • 隨著科技的進步,現有的車輛系統配備了各種不同的感測器,這使駕駛者更安全,更方便,甚至期望在未來能夠實現無人駕駛的情況。車輛系統中最重要的元素之一是導航應用。一般而言,全球導航衛星系統(GNSS)已廣泛應用於提供定位信息。然而,在許多情況下,例如市區,橋下或山區,定位結果往往不可靠。為了克服此議題,結合GNSS與INS資訊的整合導航架構被廣泛使用在車載系統中。考量到成本,系統將採用低成本慣性元件。然而為了降低成本陀螺儀產生的姿態誤差,此架構將採用雙天線系統。因此,本論文旨在開發一個基於雙天線接收機的低成本GNSS/INS改良式整合導航演算法。和傳統的演算法相比,加入了訊號評估與虛擬觀測量的應用以提升整體定位系統的強健性。並在論文的最後呈現實驗結果,並分析整合演算法與單一感測器定位的定位精度和可信度,以供未來於整合架構中感測器選擇之參考。

    With the progress of technology, the vehicles now are equipped with a variety of sensors to make driving safer, more convenient, and even automatically. One of the most critical elements in the vehicle system is the localization system. In general, the Global Navigation Satellite System (GNSS) has been widely applied to provide positioning information. However, the positioning result tends to be unreliable in situations such as urban area, under a bridge or in the mountains.
    The combination of Global Navigation Satellite System (GNSS) and Inertial Navigation System (INS) measurement data is often adopted to overcome the aforementioned issues. Under cost consideration, the low-cost IMU and dual-antenna receiver are used in the thesis. The usage of a dual-antenna receiver is to correct the attitude error from MEMS-based IMU. Therefore, the thesis aims to develop a low-cost GNSS/ INS modified integrated navigation algorithm based on a dual-antenna receiver.
    Compared with the conventional algorithm, the pseudo measurements and signal evaluation mechanism are implemented to improve the robustness. In the end, the thesis presents and analyses the experimental results.

    摘要 I Abstract II Acknowledgment IV Content V List of Figures VII List of Tables X List of Symbols XI Chapter 1. Introduction 1 1.1 Motivation 1 1.2 Objectives 1 1.3 Contribution 2 1.4 Thesis Overview 2 Chapter 2. Background 4 2.1 Coordinate System and Transformation 4 2.1.1 Coordinate System 4 2.1.2 Transformation Matrix 6 2.2 Inertial Navigation System 7 2.2.1 Inertial Measurement Unit 7 2.2.2 Strapdown Inertial Navigation System 7 2.3 Positioning Principle 9 2.3.1 Navigation Satellite Signal Measurement Model 10 2.3.2 Linearized Measurement Equation 11 Chapter 3. INS/GNSS Integration 14 3.1 Kalman Filter 14 3.2 GNSS/INS Integration Methods 15 3.2.1 Loosely-Coupled Integration 16 3.2.2 Tightly-Coupled Integration 19 3.3 Pseudo Measurements 24 3.3.1 Static Constraint 24 3.3.2 Non-Holonomic Constraint 25 3.3.3 Longitude, Latitude, and Height Constraint 26 3.3.4 Lateral Error Correlation 26 Chapter 4. Attitude Determination 27 4.1 Measurement Model 28 4.1.1 GNSS Measurement Model 28 4.1.2 GNSS-Based Attitude Determination 30 4.2 Carrier-Smoothing of Code Pseudo-range 31 4.3 Ambiguity Resolution 33 Chapter 5. Experiment and Analysis 36 5.1 Experiment Setup 36 5.1.1 Testing Field 36 5.1.2 System setup 37 5.2 Performance Analysis 43 5.2.1.1 Test 1 - Performance in the open-sky scenario 43 5.2.1.2 Test 2 - Performance in Complex Scenario 50 5.2.1.3 Test 3 - Analysis of Lateral Correction using Centerlines 58 5.2.1.4 Test 4 - Overall Performance 62 5.3 Discussion 70 Chapter 6. Conclusions 71 6.1 Conclusions 71 6.2 Future work 71 Reference 72

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