Abstract Algorithms for constructing parametric vector functions are considered to determine flight trajectories in the design calculations of flight vehicle weight parameters and flight characteristics, in the calculations of stability and required aerodynamic moments of the controlling and stabilizing surfaces when flying over the specified trajectory leg.


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    Titel :

    Design calculation of light piston-engined aircraft controllability and stability parameters


    Beteiligte:

    Erschienen in:

    Erscheinungsdatum :

    01.06.2010


    Format / Umfang :

    7 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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