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The cislunar low-thrust trajectories via the libration point

Qu, Qingyu; Xu, Ming; Peng, Kun

The low-thrust propulsion will be one of the most important propulsion in the future due to its large specific impulse. Different from traditional low-thrust trajectories (LTTs) yielded by some optimization algorithms, the gradient-based design methodology is investigated for LTTs in this paper with the help of invariant manifolds of