Application of technique described as model-controlled method (termed adaptive or semi-adaptive when applied to autopilots) for providing aircraft with variable stability and control characteristics is shown; development of variable stability helicopter using method is treated to illustrate significant design parameters and to demonstrate advantages of method over more customary approach.


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    Title :

    Model-controlled method for development of variable-stability aircraft


    Additional title:

    AGARD -- Report


    Contributors:
    Gould, D.G. (author)

    Published in:

    Publication date :

    1962


    Size :

    32 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :



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