Analysis of optical autonomous navigation for the motion of a satellite in a low-eccentricity orbit

Details Analysis of optical autonomous navigation for the motion of a satellite in a low-eccentricity orbit Analysis of optical autonomous navigation for the motion of a satellite in a low-eccentricity orbit

Nov 1985

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1985kosis..23..803i&link_type=abstract

Kosmicheskie Issledovaniia (ISSN 0023-4206), vol. 23, Nov.-Dec. 1985, p. 803-813. In Russian.

Computer Science

Numerical Analysis

Autonomous Navigation, Eccentric Orbits, Optical Communication, Satellite Orbits, Algorithms, Convergence, Error Analysis, Matrices (Mathematics), Numerical Analysis, Star Trackers

Scientific paper

A numerical algorithm and an approximate numerical-analytical method are used to examine the characteristics of an autonomous navigation system involving the application of an optical horizon star tracker. Navigation accuracy corresponding to independent and correlated measurement errors is assessed. A comparison of the two methods used shows that the approximate method makes possible a satisfactory determination of navigation errors. Navigation accuracy is evaluated for low-eccentricity orbits at altitudes from 300 to 2000 km.

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