Dataset of two-impulse Earth–Moon transfers in a four-body model

This .mat file contains data of all two-impulse Earth–Moon transfers in a four-body model generated in "On optimal two-impulse Earth–Moon transfers in a four-body model". Each row represents a solution entry, with the elements: solution achieved after MS optimization 1) transfer cost [-] 2) transfer time [-] 3) n (multiple shooting nodes) 4) ExitFlag (fmincon optimization) 5) BoundCondError (fmincon optimization) 6) t0 (initial time) [-] 7) tf (final time) [-] 8-11) initial state (x0, y0, xv0, yv0) [-] 12-15) final state (xf, yf, xvf, yvf) [-] initial guess prior MS optimization 16) alpha (angle on departure circular orbit) [-] 17) vcoeff (initial velocity coefficient) 18) t0 (initial time) [-] 19) dt (time of flight) [-] Note: instantaneous Sun angle in synodic frame equals ωs * t. Refer to the paper for the detailed description of all parameters and constants adopted to generate the dataset of solutions.