Title :
Application of Eigenspace Techniques to Design of Aircraft Control Systems
Author :
Liebst, Bradley S. ; Garrard, William L.
Author_Institution :
Department of Aerospace Engineering and Mechanics, University of Minnesota
Abstract :
Eigenspace techniques allow the control system designer to use feedback to place eigenvalues and shape eigenvectors so as to modify closed loop dynamic response characteristics to achieve performance objectives. In this paper the theory of eigenspace design is reviewed, extended and applied to several aircraft control problems.
Keywords :
Aerodynamics; Aerospace control; Aircraft; Automotive components; Control systems; Eigenvalues and eigenfunctions; Feedback control; Feedback loop; Shape control; Stability criteria;
Conference_Titel :
American Control Conference, 1985
Conference_Location :
Boston, MA, USA
