Elimination of relative secular drift of orbits of two satellites caused by polar oblateness of the Earth

Details Elimination of relative secular drift of orbits of two satellites caused by polar oblateness of the Earth Elimination of relative secular drift of orbits of two satellites caused by polar oblateness of the Earth

Feb 2011

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=2011cosre..49...65o&link_type=abstract

Cosmic Research, Volume 49, Issue 1, pp.65-71

Physics

Scientific paper

A method of elimination of relative secular drifts in satellite formations is suggested for the case of influence of a perturbation due to polar oblateness of the Earth. The method is applied to eliminate relative secular drifts in the case when a satellite is controlled using an engine mounted along its orientation axis (the satellite is supplied with a passive magnetic attitude control system) and with the help of a solar sail installed on one of the satellites. Analytical results are confirmed by numerical simulation.

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