Other
Scientific paper
Jul 1992
adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1992kosis..30..563s&link_type=abstract
Kosmicheskie Issledovaniia (ISSN 0023-4206), vol. 30, no. 4, p. 563-565.
Other
Astrometry, Circular Orbits, Orbital Position Estimation, Position Errors, Satellite Orbits, Orbital Elements, Reference Stars
Scientific paper
A system of two satellites in circular orbit is considered, with the motion parameters of one of the satellites determined from observations of the other satellite against the sky of stars (i.e., from mutual astronomic measurements). The relative position of the satellites is characterized by the angle between the radius vectors, which is optimized on the basis of the criterion of the minimum sum of coordinate error dispersions. The optimal angular distance between the satellites for position updating by this method is estimated at pi/6.
Goliakov A. D.
Smirnov Valeri V.
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