DocumentCode
486276
Title
Eigenstructure Assignment: A Tutorial - Part II Applications
Author
Sobel, K.M. ; Shapiro, E.Y.
Author_Institution
Lockheed-California Company, Burbank, CA 91520
fYear
1985
fDate
19-21 June 1985
Firstpage
461
Lastpage
467
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;
fLanguage
English
Publisher
ieee
Conference_Titel
American Control Conference, 1985
Conference_Location
Boston, MA, USA
Type
conf
Filename
4788657
Link To Document