Periodicity of motion around the collinear libration point associated with the Elliptic
Restricted Three-Body Problem is studied. A survey of periodic solutions in the Circular …

Upcoming missions and prospective design concepts in the Earth–Moon system extensively
leverage multi-body dynamics that may facilitate access to strategic locations or reduce …

Libration point orbits have been incorporated in many missions, with the capability of
orbiting near L 1 and L 2 in the Earth–Moon system recently demonstrated during the …

Trajectory design increasingly leverages multi-body dynamical structures that are based on
an understanding of various types of orbits in the Circular Restricted Three-Body Problem …

Many future satellite applications in cislunar space require repeating, periodic transfers that
shift away from some operational orbit and eventually return. Resonant orbits are …

Trajectory design increasingly leverages multi-body dynamical structures that are based on
an understanding of various types of orbits in the Circular Restricted Three-Body Problem …

A procedure has been proposed for calculating limited orbits around the L 2 libration points
of the Sun–Earth system. The motion of a spacecraft in the vicinity of the libration point has …

The research considers direct two-impulse transfers from a low-Earth orbit to circular polar
lunar orbits with an altitude of 10-15 thousand km. Such orbits are candidates for placing a …

Trajectories that exist within a multi-body dynamical environment offer low-cost options to
develop a long-term human presence within the solar system. Representing the dynamical …

В работе предлагается методика расчета ограниченных орбит вокруг точки либрации
L2 системы Солнце-Земля. Движение космического аппарата в окрестности точки …