Attitude Control of Small Scientific Satellite Using Geomagnetism

Attitude Control of Small Scientific Satellite Using Geomagnetism

Geomagnetism was used to control the attitude of the small scientific satellite at low altitude in sun-synchronous orbit. First, we analyzed the telemetry data. The rotation state of the satellite can be known from the magnitude and variations of the magnetic field which is measured from the 3 axis...

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Bibliographic Details
Main Authors:	Sung-Koo Bae, Jae-Ho Seok, Kyu-Hong Choi
Format:	Article
Language:	English
Published:	The Korean Space Science Society 1991-06-01
Series:	Journal of Astronomy and Space Sciences
Online Access:	http://ocean.kisti.re.kr/downfile/volume/kosss/OJOOBS/1991/v8n1/OJOOBS_1991_v8n1_85.pdf

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