The selenocentric orbit's formation as one of guidance problems of spacecraft with low trust which accomplishes transport tasks in the Earth-Moon system

摘要

In paper it is investigated control laws choice and suited transfer low thrust lunar-center trajectories in the Earth-Moon system in limited three-body problem. Interactive steering methodology is found. For variable initial conditions mission duration and fuel mass are obtained. It is suggested approach of initial approximation choices to solve boundary tasks. It is given results of numerical modeling.