Title :
Dynamic Output Feedback Flight Control Laws using Eigenstructure Assignment
Author :
Sobel, Kenneth M. ; Shapiro, Eliezer Y.
Author_Institution :
Lockheed California Company, Burbank, California
Abstract :
The eigenstructure assignment flight control design methodology is extended to include dynamic compensator synthesis. Dynamic compensators may be designed via eigenstructure assignment by utilizing a composite system structure. The success of this design methodology depends upon proper choice of the desired eigenvectors. An example of the lateral dynamics of an L-1011 aircraft is presented to illustrate the design method.
Keywords :
Aerospace control; Control system synthesis; Damping; Design methodology; Eigenvalues and eigenfunctions; Interconnected systems; Military aircraft; Output feedback; Stability; Time invariant systems;
Conference_Titel :
American Control Conference, 1986
Conference_Location :
Seattle, WA, USA
