Abstract:This paper proposes an application of the hybrid solar sail dynamics model in the Earth-Moon transfer orbit to achieve the design method of the reciprocal cruising orbit of solar sail spacecraft in Earth-Moon space. Based on the halo orbit invariant manifold, a strategy for hybrid solar sail dynamics conversion is established, and the theoretical methods of the three return orbits are explained. The results of simulation verification show that the hybrid solar sail can realize the reciprocal cruise orbit design based on the halo orbit invariant manifold. Compared with the traditional mission, the hybrid solar sail in this paper can reduce fuel consumption and facilitate recycling.