Problem considered is that of finding through use of observed data, coefficients of differential equations that describe dynamic system; problem occurs in determination of aerodynamic stability derivatives of airplane or missile from flight test data; free oscillation type of flight testing can never yield all coefficients; suitable forcing functions described do permit all coefficients to be evaluated.


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    Title :

    Some basic concepts for analyzing dynamic flight-test data


    Additional title:

    J Aeronautical Sciences


    Contributors:
    Klein, H. (author) / Sedney, R. (author)

    Published in:

    Publication date :

    1953


    Size :

    9 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


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