A Comparison of Averaged and Full Models to Study the Third-Body Perturbation
Figure 13
Behavior of the orbital elements for an initial inclination of 70 degrees. The values for the eccentricities 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.
