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Parametric Identification of a Return Space Vehicle during Vertical Landing
Authors:V.?A.?Afanas’ev,G.?L.?Degtyarev,A.?S.?Meshchanov  author-information"  >  author-information__contact u-icon-before"  >  mailto:mas@list.ru"   title="  mas@list.ru"   itemprop="  email"   data-track="  click"   data-track-action="  Email author"   data-track-label="  "  >Email author
Affiliation:1.South Ural State University (National Research University),Miass,Russia;2.Tupolev Kazan National Research Technical University,Kazan Tatarstan,Russia
Abstract:Real values of parameters for a space vehicle and its steering devices are specified by using the motion parameters measured in flight based on solving the differential equations of motion.
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