Optimization of circumterraneous and Interplanetary Missions of the Spacecraft with Electric Propulsion System

Аuthors

Salmin V. V.^*, Starinova O. L.^**, Volozuev V. V.^***, Petrukhina K. V.^****, Tkachenko I. S.^*****, Gogolev M. Y.^******, Chetverikov A. S.^*, Materova I. L.^*

Samara National Research University named after Academician S.P. Korolev, 34, Moskovskoye shosse, Samara, 443086, Russia

*e-mail: sputnik@ssau.ru
**e-mail: solleo@mail.ru
***e-mail: volotsuev@mail.ru
****e-mail: ksusha_10_05@mail.ru
*****e-mail: innovatore@mail.ru
******e-mail: mixa1980@mail.ru

Abstract

Design 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

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