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
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;
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
DOI :
10.1109/ICCAS.2007.4406565
