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 argument of the ascending node (rad) of the orbit considering the perturbation of the Sun and the Moon.</table>

Mathematical Problems in Engineering

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Figure 15

Figure 15: Searching for Orbits with Minimum Fuel Consumption for Station-Keeping Maneuvers: An Application to Lunisolar Perturbations 