Table 1 The initial values of the design variables by the retrograde semi-analytical 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 | − 24 | 2415 | 228 |