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 :
بازگشت