立方衛星測試用動態磁場模擬艙

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姓名

紀俊宇(Jun-Yu Ji) 查詢紙本館藏

畢業系所

光機電工程研究所

論文名稱

立方衛星測試用動態磁場模擬艙
(A dynamic magnetic field simulation cabin for cubic satellite test)

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[完整記錄]

[館藏目錄]

至系統瀏覽論文 ( 永不開放)

摘要(中)

本研究開發一個能讓衛星在地面上，模擬太空中磁場變化的磁場模擬艙。磁場模擬艙，要能抵銷機構誤差所造成的雜訊，還能抵抗外來環境磁場變化所帶來的干擾。模擬衛星磁場歷程部分，.要能自行設定軌道並取得該軌道磁場歷程。此外，雖然模擬艙內衛星為固定，亦要盡可能模擬衛星在太空中各種可能的姿態，以期重製磁場的旋轉等變化，令模擬磁場環境能更貼近真實的太空磁場變化。

摘要(英)

This study is to develop a magnetic field simulator,which satellites can measure the Earth magnetic field in space.This simulator can not only eliminate the noise caused by the mechancal error but also resist the disturbances caused by the space environment field.
When a code is written to acquire the magnetic field data along the orbit, it should output giving a Satellite magnetic field data along the Satellite path.Although the satellite is physically in the simulator,the magntic field of various satellite atitudes in space should be simulated

關鍵字(中)

★ 軌道磁場模擬

關鍵字(英)

★ Helmholtz_coil

論文目次

中文摘要 I
ABSTRACT II
目錄 IV
圖目錄 VI
第一章緒論 1
1-1 研究目的與動機 1
1-2文獻回顧 2
1-2-1Helmholtz 線圈回顧 2
1-2-2微衛星的發展，配合Helmholtz線圈，進行模擬磁場測試 3
1-2-3環境磁場與地磁、建築相關回顧 3
1-2-4定位定向硬體在廻路回顧 4
1-3 研究構想 6
1-4 論文章節 7
第二章理論及技術基礎 8
2-1 HELMHOLTZ COIL磁場均勻度定義 8
2-2 LEO衛星飛行軌道歷程計算 10
2-3 座標系統 13
2-3-1地心地固坐標系ECEF 13
2-3-2Earth-centered inertial(ECI). 13
2-3-3North east down(NED) 13
2-3-4Geographic coordinate system 14
2-3-5軌道座標 14
2-3-6衛星體座標 15
第三章系統設計 16
3-1HELMHOLTZ 程序 17
3-2大功能方塊 18
3-2-1模擬磁場建構功能方塊 18
3-2-2衛星體座標磁場次功能方塊 19
3-2-3磁場前饋回饋控制方塊 20
3-2-4 I迴路電路實現 20
3-3電流驅動磁場增益矩陣及前饋補償矩陣演算法 21
3-4PI磁場回饋演算法 23
第四章數據分析與討論 25
實驗一前饋矩陣求得及驗證 25
實驗二 PI控制 38
實驗三步階響應量測 41
實驗四衛星磁場模擬 43
第五章結論 51
REFERENCE 52

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指導教授

葉則亮

審核日期

2017-8-11

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