The multivariable control law design method of eigenstructure assignment has been in existence for a number of years. The object of the paper is to give insight into the method without too much mathematics, rather concentrating on how the method is used, and showing a number of case studies illustrating what can be achieved. The case studies use non-linear models of Vertical and Short TakeOff and Landing (VSTOL) aircraft and helicopters as a basis for the design, and show advantages and disadvantages of the method.


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    Title :

    Eigenstructure assignment in aerospace systems


    Additional title:

    Eigenstruktur Betrachtungen in Aerospace-Systemen


    Contributors:
    Smith, P.R. (author)


    Publication date :

    1989


    Size :

    , 10 Quellen


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English





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