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Parametric Identification of a Return Space Vehicle during Vertical Landing
Authors:V?A?Afanas’ev  G?L?Degtyarev  Email author" target="_blank">A?S?MeshchanovEmail author
Institution: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.
Keywords:
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