A Comparison of Averaged and Full Models to Study the Third-Body Perturbation
Figure 15
Behavior of the orbital elements for an initial inclination of 170 degrees. The values for the eccentricity are 0.01, 0.05, 0.1, 0.5, 0.7, and 0.9. The initial conditions are a = 0.341 canonical units, M 0(0) = 0, ω(0) = 0, and Ω(0) = 0.
