TsAGI Science Journal
Erscheint 6 Ausgaben pro Jahr
ISSN Druckformat: 1948-2590
ISSN Online: 1948-2604
CONTROL OF A TRAJECTORY OF A SPACE VEHICLE WITH SMALL LIFT-TO-DRAG RATIO AT DESCENT IN AN ATMOSPHERE
Volumen 43,
Ausgabe 5, 2012,
pp. 667-681
DOI: 10.1615/TsAGISciJ.2013007140
ABSTRAKT
A synthesis of descent guidance law with minimum dispersions of the terminal point is considered for the second-generation entry vehicles. The proposed law, based on the solution of inverse dynamic problem, can considerably reduce the terminal dispersions. As a prototype, the "Soyuz" spacecraft is taken.
SCHLÜSSELWÖRTER: algorithm, quasistationary gliding, nominal trajectories, area of reachability, gradient wind, statistical modeling
REFERENZIERT VON
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Vyazankin A. S., Tsvetkova N. D., Vargin P. N., Yushkov V. A., Atmospheric Modeling for Controlling the Motion of a Return Vehicle, Solar System Research, 54, 7, 2020. Crossref
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