DocumentCode
2429652
Title
Motion stability of small scale helicopter using state feedback
Author
Dharmayanda, Hardian Reza ; Kang, Taesam ; Lee, Young Jae ; Sung, Sangkyung
Author_Institution
Konkuk Univ., Seoul
fYear
2007
fDate
17-20 Oct. 2007
Firstpage
1439
Lastpage
1444
Abstract
This paper presents how to use feedback controller with helicopter state space model. We design the LQR controller to obtain controller gain matrix and used it for simulation. Our approach is simple and gives the basic understanding about how to develop controller for solving the stability of linear helicopter flight dynamics.
Keywords
aircraft control; helicopters; linear quadratic control; matrix algebra; motion control; stability; state feedback; LQR controller; controller gain matrix; feedback controller; helicopter flight dynamics; motion stability; small scale helicopter; state feedback; Aerodynamics; Aerospace control; Control system synthesis; Equations; Helicopters; Mathematical model; Stability; State feedback; State-space methods; Vehicle dynamics; LQR controller; small-scale helicopter; state space flight dynamics;
fLanguage
English
Publisher
ieee
Conference_Titel
Control, Automation and Systems, 2007. ICCAS '07. International Conference on
Conference_Location
Seoul
Print_ISBN
978-89-950038-6-2
Electronic_ISBN
978-89-950038-6-2
Type
conf
DOI
10.1109/ICCAS.2007.4406565
Filename
4406565
Link To Document