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.
Parametric Identification of a Return Space Vehicle during Vertical Landing
Russian Aeronautics ; 61 , 1 ; 23-31
2018-01-01
9 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Parametric Identification of a Return Space Vehicle during Vertical Landing
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