THE OPTIMIZATION OF INTERPLANETARY FLIGHT TO PHOBOS WITH A JET ENGINE OF COMBINED LOW AND HIGH LIMITED THRUST ArticleSamokhin A.S., Samokhina M.A., Grigoriev I.S., Zapletin M.P.Advances in the Astronautical Sciences. Том 170. 2020. С. 213-227
ПОСТРОЕНИЕ ОПТИМАЛЬНЫХ ТРАЕКТОРИЙ ЭКСПЕДИЦИЙ С ВОЗВРАЩЕНИЕМ К ЗЕМЛЕ КА С КОМБИНИРОВАННОЙ ТЯГОЙ ArticleСамохин А.С., Самохина М.А., Мамонтов Е.К., Голикова Г.Н., Горбунов Д.А."ОРБИТА МОЛОДЁЖИ" И ПЕРСПЕКТИВЫ РАЗВИТИЯ РОССИЙСКОЙ КОСМОНАВТИКИ. 2017. С. 43-44
TRAJECTORY OF THE FLIGHT TO AN ASTEROID OPTIMIZATION WITH THE USE OF EPHEMERIDES IN THE PULSE STATEMENT WITHOUT TAKING INTO ACCOUNT THE ATTRACTION OF THE EARTH ArticleМамонтов Е.К., Самохин А.С., Самохина М.А.Гагаринские чтения 2017. 2017. С. 1060-1061
OPTIMIZATION OF PHOBOS MISSION WITH HYBRID PROPULSION RETURNING TO THE EARTH ArticleGrigoryev I.S., Zapletin M.P., Samokhin A.S., Samokhina M.A.Инженерный журнал: наука и инновации. 2017. 4 с.
METHOD OF OPTIMAL TRAJECTORIES DESIGN FOR A SPACECRAFT WITH A JET ENGINE OF A LARGE LIMITED THRUST IN PROBLEMS WITH THE PHASING CONDITION ArticleSamokhina M.A., Samokhin A.S., Zapletin M.P., Grigoriev I.S.Advances in the Astronautical Sciences. Том 161. 2017. С. 711-730
OPTIMIZATION OF THE SPACECRAFT FLIGHT BETWEEN ORBITS BY SOLVING LAMBERT ArticleГоликова Г.Н., Горбунов Д.А., Самохина М.А.Гагаринские чтения 2017. 2017. С. 1055-1056