An Iterative Method of Orbit Determination from Three Observations of a Nearby Satellite

Details An Iterative Method of Orbit Determination from Three Observations of a Nearby Satellite An Iterative Method of Orbit Determination from Three Observations of a Nearby Satellite

Jun 1959

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1959saosr..27....1b&link_type=abstract

SAO Special Report #27, part 1 (1959)

Physics

2

Scientific paper

The problem of determining the orbit of a satellite from observations is
treated: (a) by disregarding the effects of air drag and perturbations
caused by the equatorial bulge - i.e., as though no perturbations exist;
(b) by considering secular perturbations caused by the bulge; and (c) by
determining corrections for atmospheric drag.

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