FORMATION OF OPTIMAL CONTROL PROGRAMS FOR LOW-THRUST SPACECRAFT FLIGHTS BETWEEN PERIODIC ORBITS RELATIVE TO LIBRATION POINTS L1 AND L2 OF THE EARTH-MOON SYSTEM
The paper studies the problem of optimal control of an electric propulsion spacecraft maneuvering between spatial periodic orbits relative to the libration points of the Earth-Moon. The flight optimization problems are solved within the framework of a restricted three-body problem, taking into account disturbances from the Sun's gravity, the non-centrality of the gravitational fields of the Earth.