DocumentCode
3504590
Title
A new tool for the analysis of modal control laws: the `pole attractors´
Author
Magni, Jean-François ; Champetier, Calixte ; Menard, Philippe
Author_Institution
CERT-DERA, Toulouse, France
fYear
1989
fDate
13-15 Dec 1989
Firstpage
1349
Abstract
In the design of modal control laws, particular attention must be devoted to the choice of the closed-loop eigenvalues. In the output feedback case, this choice becomes more and more crucial as the number of degrees of freedom appearing in the control design decreases. Then the assignment of right eigenvectors often induces weakly observable poles. The reluctance of the feedback to move away from these poles can be represented by attracting zones of the complex plane, called pole attractors. In this study the pole attractors are geometrically defined and their attractivity is quantified. The usefulness of such a concept for synthesizing modal control laws is illustrated for a realistic aircraft autopilot design
Keywords
closed loop systems; control system synthesis; eigenvalues and eigenfunctions; feedback; poles and zeros; aircraft autopilot design; closed-loop eigenvalues; complex plane; control system synthesis; eigenvectors; feedback; modal control laws; pole attractors; Actuators; Aerodynamics; Aerospace control; Aircraft; Control design; Damping; Eigenvalues and eigenfunctions; Observability; Output feedback; Time factors;
fLanguage
English
Publisher
ieee
Conference_Titel
Decision and Control, 1989., Proceedings of the 28th IEEE Conference on
Conference_Location
Tampa, FL
Type
conf
DOI
10.1109/CDC.1989.70359
Filename
70359
Link To Document