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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    Title :

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


    Contributors:

    Published in:

    Publication date :

    2010-06-01


    Size :

    7 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English




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