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研究生：	李其璋 LEE, Chi-Chang
論文名稱：	系統工程導向之教學立方衛星 System Engineering CubeSat Education Program (SECEP)
指導教授：	陳炳志 Chen, Alfred Bing-Chih
學位類別：	碩士 Master
系所名稱：	工學院 - 太空系統工程研究所 Institute of Space Systems Engineering
論文出版年：	2026
畢業學年度：	114
語文別：	中文
論文頁數：	219
中文關鍵詞：	系統工程、教學立方衛星、探空氣球、酬載整合、教學應用
外文關鍵詞：	Systems engineering, Educational CubeSat, High-altitude balloon, Space engineering education
相關次數：	點閱：17 下載：6
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SECEP（System Engineering CubeSat Education Program）是一套以實際飛行任務為教學情境，並整合軟體、硬體與教學內容之太空系統工程訓練套件，目的在於使學員能在可控的成本與開發週期下，實際參與太空任務之系統工程流程。SECEP 以探空氣球作為飛行載具，使學員可依任務目標自行設計任務酬載，在平台所提供之資源與介面條件下完成系統整合與飛行驗證。
本研究以系統工程方法進行 SECEP 之開發，由研究目標建立任務需求，再依任務執行流程逐步建立系統需求與設計規格，作為後續系統設計之依據。平台設計除需具備執行探空氣球任務所需之功能外，亦保留衛星六大次系統之代表性，使學員可藉由實際硬體理解衛星各功能間之分工與整合關係。設計過程透過系統預算分析確認平台在任務環境與資源限制下之可行性。
實際完成之 SECEP 立方衛星平台包含任務所需之電子電路系統，並整合於 1U 立方衛星機械結構中。平台提供固定之電力、資料與機械介面，以及可供學員使用之酬載空間與系統資源，使不同任務酬載能在不重新開發完整衛星平台的情況下進行設計與整合。地面段則配合飛行平台完成任務資料接收、顯示與保存，使學員得以由飛行結果進一步進行任務與系統性能分析。
在教學應用方面，本研究依太空任務生命週期建立 SECEP 訓練流程，並分別導入高中營隊與研究所課程。實際應用結果顯示，SECEP 可依學員背景與課程深度調整使用方式，使初學者能在較高引導程度下建立衛星任務概念，亦可使研究所學員以衛星平台為基礎，將精力集中於任務與酬載設計、系統整合及飛行驗證。綜合而言，SECEP 建立了一套結合系統工程方法、衛星硬體實作與高空飛行經驗之太空工程訓練平台。

SECEP, the System Engineering CubeSat Education Program, is a space systems engineering training kit that integrates hardware, software, and instructional content within the context of an actual flight mission. It is designed to provide students with hands-on systems engineering experience under manageable cost and development-cycle constraints. SECEP uses a high-altitude balloon as the flight vehicle and provides an existing educational CubeSat platform on which students can develop and integrate mission payloads according to their own objectives and available platform resources.
This study applies a systems engineering approach to derive the mission requirements, system requirements, and preliminary specifications of SECEP and subsequently transforms them into the flight-segment and ground-segment designs. Component selection and system design are supported by engineering analyses of power, data, communication, mass, and environmental conditions.
The resulting educational CubeSat platform adopts a 1U-class configuration, provides representative functions of the six major satellite subsystems, and defines the mechanical, electrical, and data interfaces required for payload integration.
A mission-life-cycle-based training process was also established and applied in both a high-school camp and a graduate-level course. The applications demonstrate that SECEP can accommodate different levels of instructional guidance while connecting systems engineering concepts, satellite hardware implementation, payload integration, and high-altitude flight experience.

摘要	ii
ABSTRACT	iii
誌謝	vii
目錄	xi
表目錄	xviii
圖目錄	xxi
第一章 緒論	1
1 研究背景	1
2 現有太空系統工程訓練平台	2
2.1 CanSat Competition	2
2.2 HEPTA-Sat與CLTP	3
2.3 綜合比較	5
3 研究目標	6
4 系統工程方法於本研究之應用	6
5 論文架構	7
第二章 任務需求	8
1 飛行任務驗證需求	8
1.1 飛行載具之初步篩選	8
1.2 無人機與探空氣球之任務適用性比較	9
1.3 SECEP 基準飛行載具之選定	10
2 衛星次系統需求	11
3 任務酬載擴充需求	11
4 商規元件與開源開發環境需求	12
5 系統工程導向課程設計需求	13
6 任務需求統整	14
第三章 系統需求與規格	16
1 本章定位與需求分析方法	16
2 任務系統邊界	17
3 任務資料需求與系統需求	18
3.1 任務資料需求	18
3.2 飛行段系統需求	20
3.3 地面段需求	25
4 細部需求	26
4.1 任務規劃需求	27
4.2 衛星平台整合與介面需求	27
4.3 衛星次系統細部需求	28
4.4 飛行段細部需求分配表	34
5 飛行段初步規格	36
5.1 上升速率	36
5.2 飛行段總吊掛重量	38
5.3 探空氣球級距與任務時間	40
5.4 視距通訊距離	43
5.5 飛行環境	45
5.6 飛行段規格統整	48
第四章 SECEP 系統設計	49
1 本章設計方法與推導流程	49
2 需求分配與設計架構建立	50
2.1 EPS 需求轉換與電力功能模組配置	50
2.2 資料流需求轉換與功能模組配置	54
2.3 結構與熱控需求轉換	59
3 OBC/C&DH 選用	61
4 感測與資料擷取元件及示範型酬載選用	64
4.2 溫度量測模組選用	67
4.3 類比數位轉換器選用	71
4.4 示範型酬載選用	72
4.5 感測元件與示範型酬載元件選用總整理	74
5 通訊鏈路設計與預算分析	75
5.1 無線通訊模組選用	75
5.2 鏈路預算分析	77
6 下行封包設計	79
6.1 平均通道佔用率限制	79
6.2 下行封包設計	80
6.3 酬載可用資料率	82
6.4 示範任務封包排程	83
6.5 SECEP 資料流架構	83
7 電力次系統設計與電力預算	85
7.1 初步功耗估算	85
7.2 電池能量需求估算	86
7.3 電池架構與型號選擇	87
7.4 太陽能板與充電管理端設計	88
7.5 DC-DC 轉換器選型與配置	90
7.6 EPS 保護與電源控制設計	92
7.7 類比數位轉換器監測點	95
7.8 電力流架構圖	97
7.9 電力預算	98
8 飛行段電路板配置與系統整合	101
8.1 硬體架構與板間介面設計	101
8.2 EPS 板配置	105
8.3 O+S 板配置	113
8.4 酬載介面板配置與酬載擴充方式	120
9 SMS/TCS 設計與重量預算	121
9.1 1U立方衛星外型設計	122
9.2 六片式外殼與拼接結構設計	123
9.3 外殼介面整合與實體組裝	125
9.4 重量預算與酬載可用空間	128
10 地面段設計	130
10.1 GS板架構	131
10.2 GS板操作區	132
11 酬載資源限制與任務耗材費用彙整	135
11.1 SECEP 基準任務條件	135
11.2 酬載資源限制總表	136
11.3 成本估算邊界與可重複使用設備	136
11.4 SECEP 衛星平台與單次任務耗材費用	137
第五章 SECEP教學設計	139
1 本章定位與教學設計目標	139
2 任務生命週期導向之教學架構	140
3 系統工程方法導入	142
3.1 系統工程基本概念建立	142
3.2 酬載作為任務需求之核心驅動	143
3.3 V-Model 與需求驗證對應關係	143
3.4 教學邏輯小結	144
4 設計審查導向之實作課程安排	144
4.1 任務籌備與系統設計	145
4.2 次系統實作與功能驗證	147
4.3 全系統整合與性能測試	150
4.4 飛行備便與任務解析	152
5 本章小結	156
第六章 SECEP教學應用成果與檢討	157
1 本章概述	157
1.1 教學應用場域	157
1.2 平台版本說明	157
1.3 本章分析重點	158
2 高中營隊課程	158
2.1 課程參與對象與背景	158
2.2 課程內容	159
2.3 教學策略	159
3 高中營隊任務成果與學員回饋	160
3.1 任務成果	160
3.2 學員回饋	162
4 研究所課程	163
4.1 課程執行方式	164
4.2 小結	165
5 研究所課程任務成果	165
5.1 高空輻射量測任務	165
5.2 臭氧量測任務	168
5.3 研究所課程成果小結	171
6 SECEP 與 HEPTA-Sat 之比較	171
6.1 比較對象與設計理念	171
6.2 平台設計與任務實作比較	172
6.3 比較結果與 SECEP 設計定位	173
7 衛星平台設計演進	174
7.1 平台演進概述	174
7.2 第一代平台	175
7.3 第二代平台	175
7.4 第三代平台	176
7.5 第四代平台改良方向	176
8 設計審查模板與課程學習矩陣建立	177
8.1 設計審查模板之內容規劃	177
8.2 課程學習矩陣	178
8.3 高中課程設計	179
8.4 大學與研究所課程設計	179
8.5 業界課程設計	179
9 本章小結	180
第七章 研究結論與未來展望	181
1 研究結論	181
2 未來展望	182
未使用生成式人工智慧代筆聲明	183
參考文獻	184
附錄A  SECEP 需求與規格彙整	191
附錄B  SECEP 酬載資源限制彙整	196
                                    

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