The response in altitude and pitching velocity of the shuttle and of four other airplanes during the landing approach is compared. The effects of airplane type, pitch damping, center-of-gravity location, lift coefficient, and cockpit position are presented. The reasons for the differences observed and the effects of these differences on control characteristics are discussed.


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    Titel :

    Altitude response of several airplanes during landing approach


    Beteiligte:

    Erscheinungsdatum :

    1979-11-01


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





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