Satellite navigation by stellar refraction

Details Satellite navigation by stellar refraction Satellite navigation by stellar refraction

Oct 1986

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1986inns.iafcs....l&link_type=abstract

IAF, International Astronautical Congress, 37th, Innsbruck, Austria, Oct. 4-11, 1986. 13 p.

Astronomy and Astrophysics

Astronomy

Atmospheric Refraction, Computerized Simulation, Satellite Navigation Systems, Star Trackers, High Altitude Balloons, Kalman Filters, Research And Development, Satellite Attitude Control

Scientific paper

An autonomous attitude control and navigation system based on the stellar refraction measurement principle is described. The system performs attitude and navigation estimation by using at least two star sensors and a three-axis gyroscope. Although the system described here is particularly adapted to a low-orbit satellite with a geocentric attitude, the principle is widely applicable. A computer simulation of the system proposed here and its hardware implementation are presented.

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