Маневры орбитальных переходов группы космических аппаратов с использованием малой тяги

Abstract

This article is dedicated about a problem of low-thrust formation and retention maneuvers for the formation flying in different conclusions including various cases within high elliptical and circular reference orbits.The thrust control, which is optimized for minimum cost of fuel was developed. To demonstrate the solution of this problem were taken different configurations maneuvers in the formation and retention of satellites.