Algebraic functions for each plane of motion, roll, pitch, and yaw, of airframe derived, assuming there is no cross coupling between planes; by use of suitable parameters they have been put in standard servomechanism form, thus assisting design and analysis of control systems for airframes.


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    Titel :

    Derivation and use of aerodynamic transfer functions of airframes


    Weitere Titelangaben:

    Roy Aeronautical Soc -- J


    Beteiligte:

    Erschienen in:

    Erscheinungsdatum :

    1955


    Format / Umfang :

    19 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



    TITANIUM IN AIRFRAMES

    KOSTOCH, F. ROBERT | SAE Technical Papers | 1953


    Welding of airframes

    Corns, W.S. | Engineering Index Backfile | 1941


    Elastomers and Airframes

    Evans, G.B. | Emerald Group Publishing | 1967


    Derivation of Aerodynamic Kernel Functions

    E.H. DOWELL AND C.S. VENTRES | AIAA | 1973