제어로봇시스템학회:학술대회논문집
- 2003.10a
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- Pages.36-40
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- 2003
Magnetic Field Correction Method of Magnetometers in Small Satellites
- Lee, Seon-Ho (Satellite Control System Dept., Korea Aerospace Research Institute) ;
- Rhee, Seung-Wu (Satellite Control System Dept., Korea Aerospace Research Institute) ;
- Ahn, Hyo-Sung (Department of Electrical Engineering, University of North Dakota)
- Published : 2003.10.22
Abstract
The considered satellite is supposed to operate in the earth-point mode and sun-point mode in accordance with the mission requirements. The magnetic field correction is based on the orbit geometry using a set of measured magnetic field data from the three-axis-magnetometer and its algorithm excludes the earth’s magnetic field model. Moreover, the usefulness of the proposed method is investigated throughout the simulation of KOMPSAT-1.