Optimal elliptic maneuvering of a spacecraft with a solar engine

• Date: 2017
• Author Affiliations: Б. М. Кiфоренко — Iнститут механiки iм. С.П.Тимошенка НАН України; Я. В. Ткаченко — Iнститут механiки iм. С.П.Тимошенка НАН України; І. Ю. Васильєв — Київський нацiональний унiверситет iменi Тараса Шевченка
• Keywords: keywords
• Main Authors: Kiforenko, B. M., Ткаченко, Я. В., Васильєв, І. Ю., Кiфоренко, Б. М.
• Format: Article
• Language: Ukrainian
• Published: Інститут математики НАН України 2017
• Online Access: https://trim.imath.kiev.ua/index.php/trim/article/view/329
• Journal Title: Transactions of Institute of Mathematics of NAS of Ukraine

The analysis of the optimal controls ensuring the minimization of the con-sumption of the working fluid of an electric propulsion (EP) of a space-craft that makes a flight between close elliptical orbits is provided. Whenmodeling the thrust of the EP, features of its generation in the plasmaEPs and...