DocumentCode
697522
Title
Desirable eigenvectors for good helicopter attitude command response handling qualities
Author
Clarke, T. ; Griffin, S.J.
Author_Institution
Dept. of Electron., Univ. of York, York, UK
fYear
2001
fDate
4-7 Sept. 2001
Firstpage
3038
Lastpage
3043
Abstract
The eigenvector structure necessary to achieve good short term attitude command response in a generic single rotor helicopter are presented. They achieve appropriate mode decoupling and are consistent with the physical relationships between the state variables. These eigenvectors translate exactly into ideal transfer functions for use with a variety of control design methodologies.
Keywords
aircraft control; attitude control; control system synthesis; eigenvalues and eigenfunctions; helicopters; rotors; transfer functions; eigenvector structure; generic single rotor helicopter; helicopter attitude command response; mode decoupling; transfer function; Aerodynamics; Aerospace control; Artificial intelligence; Eigenvalues and eigenfunctions; Equations; Helicopters; Transfer functions; Aerospace Systems; Control Applications; Design Methodologies; Vehicles and Transportation Systems;
fLanguage
English
Publisher
ieee
Conference_Titel
Control Conference (ECC), 2001 European
Conference_Location
Porto
Print_ISBN
978-3-9524173-6-2
Type
conf
Filename
7076397
Link To Document