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Due to the relative position invariance of L2 Libration point in the Earth-moon system, Halo orbits around LL2 adapt to the best mission trajectory for Lunar Relay Satellite, which can offer relay communication for space missions such as deep-space exploration and Moon outpost construction. In order to improve the payload launch capacity of Lunar Relay Satellite, the electric thrusters which have...
During the optimal design process of low-thrust transfer trajectory to translunar Libration point, the governing variable such as pitching and yaw angle of satellite were considered. However, the consideration is not enough because the selection of initial orbit after satellite-rocket separation and the inlet point of invariant manifolds are also of great importance to the transition time and the...
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