TUUSAT-1A微衛星姿態控制系統設計與分析

The Design and Analysis of Attitude Control System for Microsatellite TUUSAT-1A

黃彥臻(Yen-Jen Huang)

指導教授 ： 洪祖昌

淡江大學/工學院/機械與機電工程學系碩士班/碩士(2007年)

https://doi.org/10.6846/TKU.2007.01216

摘要

本篇摘要未授權

關鍵字

TUUSAT-1A微衛星 ； 姿態控制 ； 模擬器 ； 系統驗證計畫

並列摘要

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並列關鍵字

TUUSAT-1A Microsatellite ； Attitude Control ； Simulator ； System Verification Plan

參考文獻

[1] Fischell, R.E., ”Magnetic Damping of the Angular Motion of Earth Satellite”, America Rocket Society Journal, Vol.31 ,No.9 ,Sept.1961 ,pp.1210-1217

[2] Fischell, R.E., ”Passive Magnetic Attitude Control for Earth Satellite”, Advances in Astronautical Sciences, Vol.11 ,Jan.1962 ,pp. 147-177

[3] Chen, Yu ,”The Damped Angular Motion of a Magnetically Oriented Satellite.” Journal of The Franklin Institute, Vol.280, No.4, 1965, pp.291-306

[4] Ovchinnikov, Michael, “Attitude control system for the first Swedish nanosatellite 'MUNIN'” Acta Astronautica, v 46, n 2, 2000, p 319-326

[5] M. Yu. Ovchinnikov, “Passive Magnetic Attitude Control System of the first Russian Nanosatellite TNS-0.” Preprint of the Keldysh Institute of Applied Mathematics RAS, 2005, N 46, 23p.