A Comparison of Averaged and Full Models to Study the Third-Body Perturbation
Figure 12
Behavior of orbital elements for initial inclination of 30 degrees. The values of the eccentricity are 0.01, 0.05, 0.10, 0.50, 0.70, and 0.90. The initial conditions are a = 0.341 canonical units, M 0(0) = 0, ω(0) = 0, and Ω(0) = 0.
