Table 4 The optimal values of the design variables with the high-precision model
From: Reachable set analysis of practical trans-lunar orbit via a retrograde semi-analytic model
Design variables | \(\lambda\)/deg | \(\varphi\)/deg | \(v_{{{\text{prl}}}}\)/m/s | \(i_{{{\text{prl}}}}\)/deg |
|---|---|---|---|---|
Values | − 64.3936 | − 24.2613 | 2456.21 | 228.1633 |