Mathematical Problems in Engineering / 2013 / Article / Fig 13

Research Article

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

Figure 13

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 inclining by 28 degrees.