DocumentCode
2432308
Title
Linear-quadratic optimal model-following control of a helicopter in hover
Author
Pieper, J.K. ; Baillie, S. ; Goheen, K.R.
Author_Institution
Dept. of Mech. Eng., Calgary Univ., Alta., Canada
Volume
3
fYear
1994
fDate
29 June-1 July 1994
Firstpage
3470
Abstract
Presented are the results of a study of the application of linear quadratic optimal model following control design applied to a Bell 205 helicopter in hover. The objectives of the study were to achieve good performance and stability robustness via simulations using nominal and perturbed systems and to study the tuning procedure through extensive design analyses where effects on the closed loop system of variations in selected tuning parameters were considered.
Keywords
aircraft control; closed loop systems; helicopters; linear quadratic control; robust control; Bell 205 helicopter; aircraft control; closed loop system; linear-quadratic optimal model-following control; perturbed systems; robustness; stability; tuning procedure; Aerospace control; Aircraft; Closed loop systems; Control systems; Councils; Helicopters; Mathematical model; Optimal control; Robust stability; Tuning;
fLanguage
English
Publisher
ieee
Conference_Titel
American Control Conference, 1994
Print_ISBN
0-7803-1783-1
Type
conf
DOI
10.1109/ACC.1994.735223
Filename
735223
Link To Document