Problem is solved in principle, on basis of stability under continuously acting disturbances; theory is applied to few particular cases of longitudinal and lateral stability of aircraft; examples of calculations.


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    Title :

    Stability of partially controlled motions of aircraft


    Additional title:

    J Aerospace Sciences


    Contributors:
    Hacker, T. (author)

    Published in:

    Publication date :

    1961


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :




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