Optimization of circumterraneous and Interplanetary Missions of the Spacecraft with Electric Propulsion System
Аuthors*, **, ***, ****, *****, ******, *, *
Samara National Research University named after Academician S.P. Korolev, 34, Moskovskoye shosse, Samara, 443086, Russia
AbstractDesign and ballistic optimization methods of spacecraft missions with electric propulsion thrusters are considered. The results of different spacecraft trajectory optimization are presented.
Keywords:spacecraft; electric propulsion; thrust; optimal control; approximate methods; geocentric maneuvers; interplanetary transfer