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

Figure 13

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