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研究生： 劉容辰
Liu, Jung-Chen
論文名稱： 應用在大氣觀測微衛星之任務規劃系統
Mission Planning System for an Atmospheric Research CubeSat
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： 2017
畢業學年度： 105
語文別： 英文
論文頁數： 82
中文關鍵詞： 微衛星 、遙測與指令 、地面站 、任務規劃
外文關鍵詞： CubeSat, Telecommnad and Telemetry, Ground Station, Mission Planning
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    • 隨著電子設備的進步，微衛星所能擔負的功能也逐漸增加。從最初的姿態控制與通訊的驗證之外，開始能從事如大氣觀測等科學活動。因此衛星所需執行的任務以及地面設施間通訊的資料量也逐漸增加。但在微衛星上一些可用資源如：機載電腦記憶體或與地面通訊時間有限的情況下，我們需要利用任務規劃系統來做更有效的資源利用。
    本論文研究即是針對微衛星PHOENIX，設計一套任務規劃系統。微衛星PHOENIX為2U之微衛星並參與歐盟QB50計畫，此計畫中數個微衛星將會搭載大氣觀測科學儀器，在低地軌道形成衛星網路進行大氣研究。而任務規劃系統與演算法會以衛星操作者提供的要求為基礎並評估衛星上的機載資源與任務的重要性，規劃接下來衛星所需執行的任務以及對應的通訊指令以及執行時間。此系統將可以更有效的利用衛星上有限的資源，並大幅減少操作人員的負擔。

    The PHOENIX CubeSat is developed by NCKU as one of the CubeSats in QB50 mission which is to carry out atmospheric research within the lower thermosphere. Every CubeSat in the mission will carry atmospheric sensors as its main science payloads to collect science data which will be transmitted to the ground for science research.
    In a satellite mission, the ground station is an indispensable part because it is the only gateway to control the satellite and receive the satellite information. The operation of the ground station is governed by the mission planning system which is responsible for task scheduling and optimization. As the CubeSat missions become more complicated and diverse, the mission planning system will become more important in the CubeSat missions.
    The thesis describes the ground station and mission planning system of the PHOENIX CubeSat mission. This mission planning system can avoid the conflict between the satellite tasks, generate the telecommands scripts for the ground station software and reduce the workload of ground station operator.

    摘要 I Abstract II Acknowledgements IV Contents V List of Tables IX List of Figures X List of Abbreviations XI Chapter 1 Introduction 1 1.1 Objectives 1 1.2 Literature Study 1 1.3 Thesis organization 4 Chapter 2 PHEONIX Mission 6 2.1 QB50 mission 6 2.2 PHOENIX CubeSat 7 2.2.1 On-board data handling subsystem (OBDH) 9 2.2.2 Communication subsystem 12 2.2.3 Antenna subsystem 12 2.2.4 Electric power subsystem 13 2.2.5 Attitude determination and control subsystem 13 2.2.6 GPS receiver 13 2.2.7 Ion-Neutral Mass Spectrometer (INMS) 14 2.2.8 Solar Extreme Ultraviolet (SEUV) 14 2.2.9 Others 14 2.3 Telemetry, Tracking, and Command 15 2.3.1 System overview 15 2.3.2 Communication protocol 16 2.3.3 Telecommand packet 16 2.3.4 Telemetry packet 17 2.3.5 The list of telecommand and telemetry 18 2.3.5.1 Telecommand 20 2.3.5.2 Telemetry 23 2.4 Mission operation and requirements 25 2.4.1 Operation mode 25 2.4.2 In-Orbit operation 28 2.4.2.1 Commissioning 29 2.4.2.2 Operations 30 Chapter 3 PHOENIX Ground Station 32 3.1 System overview 32 3.2 Tracking system 33 3.2.1 Hardware 34 3.2.2 Software 34 3.3 Telemetry and Telecommand System 35 3.3.1 Hardware 36 3.3.2 Software 36 3.3.2.1 EPFL Satellite Control Software (SCS) 36 Chapter 4 Mission Planning System 39 4.1 System overview 39 4.1.1 Resource 39 4.1.1.1 The communication with ground station 40 4.1.1.2 Power 41 4.1.1.3 Memory 41 4.1.2 Mission scenario 42 4.2 System design 43 4.3 Software function 44 4.3.1 Priority define 44 4.3.2 Satellite simulator 45 4.3.3 Task definition 46 4.3.4 Mission planning algorithm 47 4.3.5 Telecommand optimized 49 4.3.6 Convert task to telecommand 50 4.3.7 Create telecommand script 50 Chapter 5 Testing and Verification 52 5.1 Testing configuration 52 5.1.1 Hardware 52 5.1.2 Software 56 5.2 Testing campaign 57 5.2.1 Testing on ground station 57 5.2.1.1 End to end test 57 5.2.1.2 Mission verification test 58 5.2.1.3 Telecommand test 58 5.2.1.4 End-to-end test with in-orbit satellite 58 5.2.2 Testing on satellite planning test 58 5.2.2.1 Scenarios testing 59 5.2.2.2 Testing with PHOENIX 60 5.3 Testing result 60 5.3.1 Test result of end-to-end test 61 5.3.2 Test result of scenarios testing 62 5.3.3 Test result of testing with PHOENIX 72 Chapter 6 Conclusion and Future Works 76 6.1 Summary 76 6.2 Future work 77 Reference 78

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