Title :
Eigenstructure Assignment: A Tutorial - Part II Applications
Author :
Sobel, K.M. ; Shapiro, E.Y.
Author_Institution :
Lockheed-California Company, Burbank, CA 91520
Abstract :
A tutorial description of the application of eigenstructure assigment to flight control system design is presented. Both output feedback and constrained output feedback are considered. Examples include a stability augmentation system, an autopilot, and decoupled mode control.
Keywords :
Aerospace control; Aircraft; Attitude control; Control systems; Equations; Filters; Output feedback; Shape control; Stability; Tutorial;
Conference_Titel :
American Control Conference, 1985
Conference_Location :
Boston, MA, USA
