Analytical and flight simulator studies were conducted to examine effects on selection of optimum longitudinal control sensitivity of oscillatory mode dynamics, certain stability derivatives, and level of turbulence; improved method for presenting optimum control sensitivity criteria is discussed which has promise as means for correlating flight-test data for aircraft having widely different aerodynamic, mass, and inertia characteristics; further studies are planned at United Aircraft Corp in which approach will be used to develop methods for presenting criteria for minimum satisfactory control sensitivity and control power.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Research on VTOL aircraft handling qualities criteria


    Additional title:

    J Aircraft


    Contributors:
    Miller, D.P. (author) / Clark, J.W. (author)

    Published in:

    Publication date :

    1965


    Size :

    8 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :