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Статья поступила в редакцию 23.06.2014
Соколов Николай Леонидович — канд. техн. наук, старший научный сотрудник, за-
меститель начальника ЦУП ЦНИИмаш.
ФГУП ЦНИИмаш, Российская Федерация, 141070, Московская обл., г. Корол¨eв,
ул. Пионерская, д. 4.
Sokolov N.L. — Ph.D. (Eng.), Senior Researcher, Deputy Director of the Mission Control
Centre of the Federal State Unitary Enterprise The Central Research Institute for Machine
Building.
Federal Unitary State Enterprise Central Research Institute for Machine Building,
ul. Pionerskaya 4, Korolev, Moscow Region, 141070 Russian Federation.
Просьба ссылаться на эту статью следующим образом:
Соколов Н.Л. Оптимальное управление космическим аппаратом на участке пред-
варительного аэродинамического торможения при выведении на орбиту искусствен-
ного спутника Марса // Вестник МГТУ им. Н.Э. Баумана. Сер. Машиностроение.
2015. № 6. C. 4–21.
Please cite this article in English as:
Sokolov N.L. Spacecraft optimal control in drag braking flight segment during insertion
into orbit of Mars artificial satellite.
Vestn. Mosk. Gos. Tekh. Univ. im. N.E. Baumana,
Mashinostr.
[Herald of the Bauman Moscow State Tech. Univ., Mech. Eng.], 2015, no. 6,
pp. 4–21.
ISSN 0236-3941. Вестник МГТУ им. Н.Э. Баумана. Сер. “Машиностроение” 2015. № 6 21