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 semimajor axis of the orbit (m) considering the perturbations of the Sun and the Moon for orbits beyond the Moon.</table>

Mathematical Problems in Engineering

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Figure 6

Figure 6: Searching for Orbits with Minimum Fuel Consumption for Station-Keeping Maneuvers: An Application to Lunisolar Perturbations 