Path: Interplanetary/LowEnergyManeuver
% Compute a periodic orbit for a LET transfer. The orbit has nearest periapsis at r1. Loads the corresponding mat-files to the selected family: f16, f17, f18, f19, f20, and f26. If desired will save updated data to mat-files. Type IteratePeriodicOrbit for a demo. -------------------------------------------------------------------------- Form: d = IteratePeriodicOrbit( p1, mu, family ) -------------------------------------------------------------------------- ------ Inputs ------ mu (1,1) Gravity ratio of the CRTBP p1 (1,1) Nearest periapse radius family (1,:) Family name from Markellos catalog e.g. 'f16','f16p' doSave (1) Whether to save data ------- Outputs ------- d (:) Data structure with information about the orbit --------------------------------------------------------------------------