Autonomous navigation of a geostationary satellite according to measurements with low information content

Details Autonomous navigation of a geostationary satellite according to measurements with low information content Autonomous navigation of a geostationary satellite according to measurements with low information content

Jan 1988

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1988kosis..26..154k&link_type=abstract

Kosmicheskie Issledovaniia (ISSN 0023-4206), vol. 26, Jan.-Feb. 1988, p. 154-157. In Russian.

Astronomy and Astrophysics

Astronomy

Autonomous Navigation, Geosynchronous Orbits, Orbit Perturbation, Space Navigation, Astrodynamics, Dynamic Models, Spherical Coordinates

Scientific paper

A fast algorithm is developed which provides for high accuracy of autonomous navigation for a geostationary satellite. The algorithm is based on the use of analytical formulas for quasi-circular motion, a quasi-linear Kalman filter, and an optimal strategy for the measurement of the navigation parameters. RMS errors of the estimation of satellite orbit period are determined in the framework of the proposed approach.

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