Trajectory Control for a Spacecraft with an Inflatable Braking Device in the Martian Atmosphere |
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| Authors: | Aleksashkin S. N. Bobylev A. V. Vlasenko O. V. Pichkhadze K. M. Terterashvili A. V. Yaroshevsky V. A. |
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| Affiliation: | (1) Babakin Research Center, Moscow, Russia;(2) Zhukovsky Central Aerohydrodynamical Institute, Zhukovsky, Moscow oblast, Russia |
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| Abstract: | The possibility of using an inflatable braking device for controlled descent in the Martian atmosphere of large-capacity cargoes is analyzed. The most complicated version of the trajectory control problem is considered, namely, the injection of a spacecraft at hyperbolic velocity into a parking orbit after braking in the atmosphere. |
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