The eigenstructure assignment flight control design methodology is extended to include dynamic compensator synthesis. Dynamic compensators may be designed via eigenstructure assignment by utilizing a composite system structure. The success of this design methodology depends upon proper choice of the desired eigenvectors. An example of the lateral dynamics of an L-1011 aircraft is presented to illustrate the design method.
Dynamic output feedback flight control laws using eigenstructure assignment
Rueckgekoppelte, dynamische Ausgangs-Flugregelfunktion mit Eigenstruktur-Zuteilung
Proc. of the 1986 American Control Conf. ; 1 ; 605-610
1986
6 Seiten, 3 Bilder, 10 Quellen
Aufsatz (Konferenz)
Englisch
Eigenstructure Assignment using Output Feedback
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