The Study of the Asymmetric Multiple Encounters Problem and Its Application to Obtain Jupiter Gravity Assisted Maneuvers

Figure 14

Variation of energy (Δ𝐸) obtained by the swing-by in the situation where 𝑒=0.9, −2.5≤𝜓_𝑜≤3.5 rad, and −2.5≤𝜓_𝑓≤3.5 rad.