DocumentCode
2660496
Title
Flight control of a VSTOL aircraft using polynomial eigenstructure assignment
Author
White, B.A.
Volume
2
fYear
1996
fDate
2-5 Sept. 1996
Firstpage
758
Abstract
The paper describes the method of polynomial eigenstructure assignment and its application to a multivariable VSTOL aircraft. The theory of polynomial eigenstructure assignment is described, together with the controller structure. Metrics are described that evaluate interaction, actuator motion and robustness.
Keywords
MIMO systems; aircraft control; closed loop systems; compensation; eigenstructure assignment; poles and zeros; polynomials; robust control; velocity control; VSTOL aircraft; actuator motion; controller structure; flight control; interaction; polynomial eigenstructure assignment; robustness;
fLanguage
English
Publisher
iet
Conference_Titel
Control '96, UKACC International Conference on (Conf. Publ. No. 427)
ISSN
0537-9989
Print_ISBN
0-85296-668-7
Type
conf
DOI
10.1049/cp:19960647
Filename
656022
Link To Document