Paper Title :Development of LQR Controller Design for Small Unmanned Aerial Vehicle
Author :Hteik Tin Cho Nyunt, Hla Myo Tun, Thanda Win
Article Citation :Hteik Tin Cho Nyunt ,Hla Myo Tun ,Thanda Win ,
(2018 ) " Development of LQR Controller Design for Small Unmanned Aerial Vehicle " ,
International Journal of Electrical, Electronics and Data Communication (IJEEDC) ,
pp. 1-7,
Volume-6,Issue-6
Abstract : UAV have been increasingly developed in war wide. The LQR controller for Small UAV is designed in this
paper. The Linear Quadratic Regulator (LQR) design for analyzing the stable condition of UAV is very important role in
unmanned system with optimal control. Unmanned Aerial Vehicle (UAV) will be designed by LQR controller. A controller
is designed based on Linear Quadratic Regulator Theory by using “LQR” and “regulator” functions from MATLAB. The
MATRIX function is used to evaluate the dynamic stability of the aircraft model. Linear and non-linear controllers for the
stabilization of attitude of the vehicle and control of its altitude have been designed and implemented via simulation. The
design process and tools investigated in this paper allow the designer to obtain the LQR controller, model the closed-loop
plant/controller system, and evaluate the controller’s performance using MATLAB. There are three situations to test the
stability analysis with open-loop, without noise condition and with additional noise condition. Using this model, the control
system response to commanded inputs and external disturbance must be evaluated.
Keywords - Small UAV, LQR Controller Design, Stability Analysis, Control Techniques, MATLAB
Type : Research paper
Published : Volume-6,Issue-6
DOIONLINE NO - IJEEDC-IRAJ-DOIONLINE-12586
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Copyright: © Institute of Research and Journals
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Published on 2018-08-13 |
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