DocumentCode
486278
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
fYear
1985
fDate
19-21 June 1985
Firstpage
475
Lastpage
480
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;
fLanguage
English
Publisher
ieee
Conference_Titel
American Control Conference, 1985
Conference_Location
Boston, MA, USA
Type
conf
Filename
4788659
Link To Document