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New periodic orbits in the solar sail restricted three body problem

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Figure

Fig. 1.The rotating coordinate frame and the sail position therein. The angles γ andφ which the sail normal makes with respect to the rotating frame are also shown.
Fig. 2.Surfaces of equilibrium points in thespecified by a constant value of xe-ze parameter space
Fig. 3.A family of orbits witha different equilibrium point along the β = 0.05. Each orbit has the same amplitude and is about β level curve shown in Figure 2, each equilibriumpoint being defined by a different γ value
Fig. 4.Periodic Orbits in the rotating-pulsating frame: the thin line orbit is for e = 0and the thick lined orbit is for e = 0.0167

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