Исследование точностных характеристик комплекса алгоритмов терминального наведения перспективного пилотируемого космического корабля на конечном участке спуска в атмосфере Земли

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С.И. Кудрявцев
12 Инженерный журнал: наука и инновации # 32016
[10] Kudryavtsev S.I. Identifikatsiya parametrov modeli spuskaemogo apparata pri
radioupravlenii v atmosfere Zemli [Determining the parameters of a landing
module model for radio guidance in the Earth’s atmosphere]. Sb. RKT [Rocket
and Space Technology Miscellany], TsNIImash Publ., 1984, ser. XI, no. 1.
Available at:
[11] Kudryavtsev S.I., Savchenko A.A. Avtomatizirovannyy kompleks programm
rascheta spuskov korabley “Soyuz TM” i ”Progress M” [Automated
computational software package for Soyuz TM and Progress M spacecraft
deorbiting]. Sb. RKT [Rocket and Space Technology Miscellany], TsNIImash
Publ., 1991, ser. IX, no. 2. Available at:
Kudryavtsev S.I. (b. 1959) graduated from the Moscow Forest Engineering Institute
(Moscow State Forest University) in 1981. Cand. Sci. (Eng.), Head of the Laboratory,
Federal State Unitary Enterprise TsNIIMash, Assoc. Professor, Department of Automated
Control Systems, Moscow State Forest University. Author and co-author of over 70 sci-
entific publications in the fields of design ballistics and ballistic and navigation support
of spacecraft deorbiting. e-mail: