Search Results - "Lavrenov, S M"

Celestial-mechanical interpretation of the two-way radio measurements of radial velocity of spacecraft for scientific applications by Komovkin, S. V., Lavrenov, S. M., Tuchin, A. G., Tuchin, D. A., Yaroshevsky, V. S.

“…The article describes a model of the two-way measurements of radial velocity based on the Doppler effect. The relations are presented for the instantaneous…”
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Ballistics, navigation, and motion control for a spacecraft during its landing on the surface of Phobos by Akim, E. L., Arkhangelsky, R. N., Zaiko, Yu. K., Lavrenov, S. M., Poroshin, A. L., Ruzsky, E. G., Stepaniants, V. A., Tuchin, A. G., Tuchin, D. A., Fedotov, V. P., Yaroshevsky, V. S.

“…Basic concepts and algorithms laid as foundations of the scheme of landing on the Martian moon Phobos (developed for the Phobos-Grunt project) are presented…”
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Adaptive Methods of the Flybys Constructing in the Jovian System with the Orbiter Insertion Around the Galilean Moon by Golubev, Yu. F., Grushevskii, A. V., Koryanov, V. V., Lavrenov, S. M., Tuchin, A. G., Tuchin, D. A.

“…— We consider space expeditions with a long-term spacecraft stay near the studied celestial body (artificial satellites of small bodies of the Solar System),…”
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Ballistic design of transfer trajectories from artificial-satellite earth orbit to halo orbit in the neighborhood of the L2 point of the Sun-Earth system by Il’in, I. S., Zaslavsky, G. S., Lavrenov, S. M., Sazonov, V. V., Stepanyantz, V. A., Tuchin, A. G., Tuchin, D. A., Yaroshevsky, V. S.

“…The paper considers the ballistic design of spacecraft (SC) transfer to the neighborhood of the L 2 point and subsequent entry of the SC into the halo orbit…”
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Ballistic design of transfer trajectories from artificial-satellite earth orbit to halo orbit in the neighborhood of the L 2 point of the Sun-Earth system by Il’in, I. S., Zaslavsky, G. S., Lavrenov, S. M., Sazonov, V. V., Stepanyantz, V. A., Tuchin, A. G., Tuchin, D. A., Yaroshevsky, V. S.

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Ballistic design of transfer trajectories from artificial-satellite earth orbit to halo orbit in the neighborhood of the L^sub 2^ point of the Sun-Earth system by Il'in, I S, Zaslavsky, G S, Lavrenov, S M, Sazonov, V V, Stepanyantz, V A, Tuchin, A G, Tuchin, D A, Yaroshevsky, V S

“…The paper considers the ballistic design of spacecraft (SC) transfer to the neighborhood of the L ^sub 2^ point and subsequent entry of the SC into the halo…”
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Ballistic design of transfer trajectories from artificial-satellite earth orbit to halo orbit in the neighborhood of the L sub(2) point of the Sun-Earth system by Il'in, I S, Zaslavsky, G S, Lavrenov, S M, Sazonov, V V, Stepanyantz, V A, Tuchin, A G, Tuchin, DA, Yaroshevsky, V S

“…The paper considers the ballistic design of spacecraft (SC) transfer to the neighborhood of the L sub(2) point and subsequent entry of the SC into the halo…”
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