A novel type of ER3BP introducing Milankovitch cycles or seasonal irradiation processes influencing onto orbit of planet

摘要

Abstract A developing approach for solving equations of a trapped motion of small satellite near the secondary planet mplanet (Earth) in case of the elliptic restricted problem of three bodies, ER3BP, is presented hereby. In ordinary way, this problem includes consideration of two primaries, MSun and mplanet (mplanet?