Mathematical Problems in Engineering / 2013 / Article / Fig 6

Research Article

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

Figure 6

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.