次軌道任務用立方衛星姿態控制系統開發

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姓名

王嘉(Chia Wang) 查詢紙本館藏

畢業系所

光機電工程研究所

論文名稱

次軌道任務用立方衛星姿態控制系統開發
(Development of the attitude control system of the cubic satellite for suborbital mission)

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摘要(中)

本論文目的為開發皮、奈米衛星等級衛星於次軌道任務中使用的姿態控制系統，使用商業現成元件製成的動量輪為姿態致動器，並整合地磁計、陀螺儀及地弧感測器數據判定姿態。衛星預期以混合式火箭為載具，探測位於高空一百公里至三百公里處的電離層不規則體，於高空脫離後利用本模組減滾並提供儀器之指向。研究已開發完成系統之機構、驅動電路及控制軟體，並設計扭力測試量測動量輪之角動量容量、旋轉測試驗證衛星之減滾及姿態控制流程。

摘要(英)

The purpose of this paper is to develop an attitude determination and control system (ADCS) for pico and nano-satellite at sub-orbital task. The actuator　of this system is momentum wheel which made by commercial-off-the-shelf (COTS) components. And data of geomagnetic, gyroscope and earth sensor is integrated to determine the attitude. A hybrid rocket is expected to be the carrier of satellite, probing the irregularities of ionosphere at 100km to 300km altitude. After satellite detached form carrier, this module provides de-spin and instruments pointing ability. In this research, mechanical structure, circuit and control software have been developed. A torque test has performed to determine capacity of momentum wheel, and a rotation test has performed for validation of attitude control and de-spin process.

關鍵字(中)

★ 姿態控制
★ 動量輪
★ 次軌道任務

關鍵字(英)

論文目次

第一章緒論 1
1-1 研究目的與動機 1
1-2文獻回顧 3
1-3 研究構想 5
1-4 論文章節 7
第二章研究背景 8
2-1理論基礎 8
2-1-1慣性參考座標 8
2-1-2 體座標 9
2-1-3方向餘弦矩陣 10
2-1-4尤拉角 11
2-1-5四元數 14
2-2技術背景 17
2-2-1無刷直流馬達驅動原理 17
第三章系統設計 19
3-1系統需求及周邊環境 19
3-2功能方塊 20
3-2-1全系統 20
3-2-2姿態感測 21
3-2-3動量輪 23
3-2-4電源保護 25
3-3狀態機械 26
3-3-1姿態感測次系統狀態機械 26
3-3-2動量輪控制次系統狀態機械 28
3-4具體實現 29
3-4-1機構設計 29
3-4-2電路設計 34
第四章實驗設計 44
4-1有無感測器控制性能測試 44
4-2 動量輪角動量測試 50
4-3 減滾測試 57
第五章結論 61
參考文獻 62

參考文獻

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[3] Bleier, Thomas, and C. Dunson. "ELF magnetic field monitoring of the San Simeon M6. 4 quake from both Quakesat and a ground network." Proceedings of the International Workshop on Seismo-Electromagnetics, Tokyo, Japan, March, 2005.
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[7] Kayal, H., Baumann, F., Briess, K., and Montenegro, S., “Beesat: A pico satellite for the on orbit verification of micro wheels.” Recent Advances in Space Technologies, RAST′07. 3rd International Conference , pp. 497-502, 2007
[8] Xiang, T., Meng, T., Wang, H., Han, K., and Jin, Z. H. “Design and on-orbit performance of the attitude determination and control system for the ZDPS-1A pico-satellite”, Acta Astronautica, 77, pp. 182-196, 2012.
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[12] Kuipers, Jack B. Quaternions and rotation sequences, Princeton: Princeton university press, 1999.
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指導教授

江士標

審核日期

2014-7-18

推文