In this paper, kinematic synthesis of a planar flight control system mechanism has been conducted for a light aircraft designed and built by TAI. To achieve a simple construction, the four-bar linkages are used in the synthesis. Freudenstein's Method and Bloch's Method are utilized for analytical three and four bar position syntheses respectively. A case study of an elevator flight control system is presented.


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    Titel :

    Kinematic synthesis of flight control systems for light aircrafts


    Beteiligte:
    Yaman, Yavuz (Autor:in) / Akman, Yunus (Autor:in) / Söylemez, Eres (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    2002-02-01


    Format / Umfang :

    7 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch






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