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.
Eigenstructure assignment in aerospace systems
Eigenstruktur Betrachtungen in Aerospace-Systemen
IEE Colloquium on 'Navigation, Guidance and Control on Aerospace' ; No.142 ; 5/1-5/6
1989
, 10 Quellen
Conference paper
English
Eigenstructure assignment for aerospace applications: MATLAB implementation
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