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CONTROL OF A TRAJECTORY OF A SPACE VEHICLE WITH SMALL LIFT-TO-DRAG RATIO AT DESCENT IN AN ATMOSPHERE

Volumen 43, Edición 5, 2012, pp. 667-681
DOI: 10.1615/TsAGISciJ.2013007140
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SINOPSIS

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.

CITADO POR
  1. 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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