Elimination of relative secular drift of orbits of two satellites caused by polar oblateness of the Earth
- First Online:
- Cite this article as:
- Ovchinnikov, M.Y. & Zaramenskikh, I.E. Cosmic Res (2011) 49: 65. doi:10.1134/S0010952511010059
- 36 Downloads
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.