Title :
Improved observer design incorporating modal consideration
Author :
Shapiro, E.Y. ; Silverman, L.M.
Author_Institution :
Lockheed California Co., Burbank, CA
Abstract :
A method for designing observers which utilizes state disturbance information is given. This approach is a natural dual to the control eigenvalue/eigenvector placement design.
Keywords :
Aerospace control; Control systems; Design methodology; Eigenvalues and eigenfunctions; Feedback control; Linear feedback control systems; Noise measurement; State feedback; Time invariant systems; Vectors;
Conference_Titel :
Decision and Control including the Symposium on Adaptive Processes, 1981 20th IEEE Conference on
Conference_Location :
San Diego, CA, USA
DOI :
10.1109/CDC.1981.269356
