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Problemy Upravleniya, 2010, Issue 6, Pages 58–63 (Mi pu618)  
Control the moving objects and navigation

Features of ballistics and navigation solutions for descent used in the control system of the manned transport spacecraft “Soyuz TMA”

E. A. Mikrin, L. I. Komarova, I. V. Orlovsky, S. N. Evdokimov, A. I. Lukashevich

S. P. Korolev Rocket and Space Corporation "Energia", Korolev
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Abstract: Problems of autonomous ballistics and navigation support for descent of the “Soyuz TMA” descent vehicle onto the given ground are considered. Structures and features of onboard algorithms to determine navigation state vector are described. Methods of calculations necessary for descent in cases of emergency are presented.
Keywords: transport piloted vehicle, descent module, autonomous ballistics and navigation support for descent.
Document Type: Article
UDC: 629.78
Language: Russian
Citation: E. A. Mikrin, L. I. Komarova, I. V. Orlovsky, S. N. Evdokimov, A. I. Lukashevich, “Features of ballistics and navigation solutions for descent used in the control system of the manned transport spacecraft “Soyuz TMA””, Probl. Upr., 2010, no. 6, 58–63
Citation in format AMSBIB
\Bibitem{MikKomOrl10}
\by E.~A.~Mikrin, L.~I.~Komarova, I.~V.~Orlovsky, S.~N.~Evdokimov, A.~I.~Lukashevich
\paper Features of ballistics and navigation solutions for descent used in the control system of the manned transport spacecraft ``Soyuz TMA''
\jour Probl. Upr.
\yr 2010
\issue 6
\pages 58--63
\mathnet{http://mi.mathnet.ru/pu618}
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