Searching for Orbits with Minimum Fuel Consumption for Station-Keeping Maneuvers: An Application to Lunisolar Perturbations

<table>Perturbation integral (m/s) as a function of the inclination (rad) of the orbit considering the perturbation of the Sun and the Moon with the orbit of the Moon inclined by 18 degrees.</table>

Mathematical Problems in Engineering

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Figure 12

Figure 12: Searching for Orbits with Minimum Fuel Consumption for Station-Keeping Maneuvers: An Application to Lunisolar Perturbations 