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

Figure 10

Perturbation integral (m/s) as a function of the inclination (rad) of the orbit considering the perturbation of the Moon for inclinations of the orbit of the Moon of 18 degrees (dotted line), 23 degrees (dashed line), and 28 degrees (continuous line).