Использование в оперативном контуре управления космическим аппаратом перспективного алгоритма выбора наиболее безопасного варианта спуска при возникновении нештатной ситуации

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А.Ю. Кутоманов, С.И. Кудрявцев
10 Инженерный журнал: наука и инновации # 22016
Problems of using a prospective selection algorithm
in the operational control loop for maximum descent
safety in case of off-nominal situations
© . Kutomanov, S.I. Kudryavtsev
Federal State Unitary Enterprise TsNIIMash, Korolyov, 141070, Russia
The article considers problems of promptly ensuring a safe deorbiting of the crew in case
of an emergency descent. Analysis of relevance of developing a deorbiting safety algo-
rithm for cases when landing onto standard grounds is impossible is presented. Basic
requirements for a deorbiting guidance system of prospective manned spacecraft neces-
sary for the algorithm operation are shown. Results of updating the deorbiting safety
algorithm for it to function in the operational control loop are presented.
Keywords: combined guidance system, precision landing guidance, satellite navigation,
crew safety.
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Kutomanov (b. 1988) graduated from Bauman Moscow State Technical Universi-
ty in 2011. Deputy Head of Department, Federal State Unitary Enterprise TsNIIMash.
Author and co-author of over 20 scientific publications in the fields of design ballistics
and ballistic and navigation support of spacecraft deorbiting.
e-mail: