Title :
Eigenstructure assignment, eigensensitivity, and flight control design
Author :
Sobel, K.M. ; Shapiro, E.Y.
Author_Institution :
Lockheed California Company, Burbank, CA
Abstract :
A sensitivity measure which describes changes in the damping of complex conjugate eigenvalues due to changes in the entries of the closed loop system matrix is introduced. An example is presented to illustrate the application of eigenstructure assignment with damping sensitivity reduction to the design of a flight control system.
Keywords :
Aerospace control; Aircraft; Closed loop systems; Damping; Design methodology; Digital signal processing; Eigenvalues and eigenfunctions; Equations; Output feedback; Uncertain systems;
Conference_Titel :
Decision and Control, 1985 24th IEEE Conference on
Conference_Location :
Fort Lauderdale, FL, USA
DOI :
10.1109/CDC.1985.268575
