The dynamics of solar-sail maneuvers are conceptually different from classical control maneuvers where one considers impulsive changes in the velocity of a spacecraft. Solar-sail orbits are continuous in both position and velocity in a varying vectorfield, opening the possibility of the existence of heteroclinic connections by means of artificially changing the vectorfield with a sail maneuver. This paper investigates solar-sail assisted maneuvers to obtain families of artificial heteroclinic connections between Lissajous libration point orbits. The study is based on a careful analysis of the geometry of the phase space of the linearized equations around the equilibrium points, the dynamical identification of the main parameters and the representation of the solutions in the action-angle variables. We identify the main dynamical properties of the connecting families presenting systematic new options for the mission analysis in the libration point regime using this technology, including a methodology to approach the classical problem of exclusion zone avoidance.

太阳帆操纵的动力学在概念上不同于经典的控制操纵，在经典的控制操纵中，人们考虑了航天器速度的脉冲变化。太阳帆轨道在变化的矢量场中在位置和速度上都是连续的，从而通过人工操纵帆来改变矢量场，从而开启了存在异斜连接的可能性。本文研究了太阳帆辅助演习，以获取李沙育解放点轨道之间的人工杂斜连接族。该研究基于对平衡点周围线性方程组相空间几何形状的仔细分析，主要参数的动力学识别以及作用角变量中解的表示形式。