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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    Title :

    Parametric Identification of a Return Space Vehicle during Vertical Landing


    Contributors:

    Published in:

    Russian Aeronautics ; 61 , 1 ; 23-31


    Publication date :

    2018-01-01


    Size :

    9 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English




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