Control of a spacecraft’s spatial turn with minimum value of the path functional

By Levskii M.  

Cosmic Research, Vol. 45, Iss. 3, 2007-06 ,pp. : 234-247

MAIK Nauka/Interperiodica

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The use of solutions to problems of spacecraft trajectory optimization in impulse formulation when solving the problems of optimal control of trajectories of a spacecraft with limited thrust engine: I

By Grigoriev I.   Grigoriev K.  

Cosmic Research, Vol. 45, Iss. 4, 2007-08 ,pp. : 339-347

MAIK Nauka/Interperiodica

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An Effective Algorithm of Aerodynamic Control over Spacecraft Descent

By Shcherban' I.  

Cosmic Research, Vol. 43, Iss. 6, 2005-11 ,pp. : 450-455

MAIK Nauka/Interperiodica

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Pyromechanical and detonation systems of construction separation in spacecraft for planetary and astrophysical investigations

By Efanov V.   Moisheev A.   Pichkhadze K.  

Cosmic Research, Vol. 44, Iss. 3, 2006-05 ,pp. : 220-225

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Application of information criteria to control the structurally uncertain navigation system of a reusable spacecraft

By Pogorelov V.  

Cosmic Research, Vol. 47, Iss. 1, 2009-02 ,pp. : 44-52

MAIK Nauka/Interperiodica

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