Attitude Determination of Micro-Satellite Using Geomagnetism and Magnetometer Data

Details Attitude Determination of Micro-Satellite Using Geomagnetism and Magnetometer Data Attitude Determination of Micro-Satellite Using Geomagnetism and Magnetometer Data

Dec 1992

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1992jass....9..203s&link_type=abstract

Journal of Astronomy and Space Sciences, vol.9, no.2, p.203-212.

Astronomy and Astrophysics

Astronomy

Scientific paper

Geomagnetic data from 3-axis magnetometer and the IGRF model(tilted-eccentric dipole model) were used to determine the attitude of a satellite. We compared the values of the geomagnetic model with the magnetometer data and two attitude angles, called ¥á-angle and ¥â-angle respectively, were calculated. From these angles we calculated simple bounds, ¥ã1 and ¥ã2, on the true attitude angle ¥ã, which is used to detemine attitude, between the z-axis and the local vertical. And then we investigated conditions of attitudes of UoSAT-11, 14, 22.

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