This paper uses the concepts of output and input coupling to provide a complete approach to design by eigenstructure assignment, by considering both the left and right eigenvectors. These concepts are illustrated by consideration of the design of a controller for a VSTOL aircraft in the transition flight regime. Results are presented for both the linear and nonlinear aircraft representations.
Use of eigenstructure assignment in VSTOL aircraft control law design
Die Benutzung der Eigenstrukturzuordnung beim Entwurf der Steuerungsgesetze für ein VSTOL-Flugzeug
International Conference on Control ' ; 2 ; 1028-1034
1991
7 Seiten, 14 Quellen
Aufsatz (Konferenz)
Englisch
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