Flight testing of the Space Shuttle Orbiter is in progress and current results of the post-flight aerodynamic analyses are discussed. The purpose of these analyses is to reduce the pre-flight aerodynamic uncertainties, thereby leading to operational certification of the Orbiter flight envelope relative to the integrated airframe and flight control system. Primary data reduction is accomplished with a well documented maximum likelihood system identification techniques.


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    Titel :

    Stability and control flight test results of the space transportation system's orbiter


    Beteiligte:
    Culp, M. A. (Autor:in) / Cooke, D. R. (Autor:in)

    Kongress:

    Atmospheric Flight Mechanics Conference ; 1982 ; San Diego, CA


    Erscheinungsdatum :

    1982-08-01


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :