IJEEDC Modelling and PID Control System for Fixed-Wing Unmanned Aerial Vehicle

Journal Paper

Paper Title :Modelling and PID Control System for Fixed-Wing Unmanned Aerial Vehicle

Author :Thanda Win, Hla Myo Tun, Hteik Tin Cho Nyunt

Article Citation :Thanda Win ,Hla Myo Tun ,Hteik Tin Cho Nyunt , (2018 ) " Modelling and PID Control System for Fixed-Wing Unmanned Aerial Vehicle " , International Journal of Electrical, Electronics and Data Communication (IJEEDC) , pp. 8-11, Volume-6,Issue-6

Abstract : The paper focuses on the PID control techniques a for small UAV. In this research work, control derivatives were implemented for analytical method for longitudinal dynamics of a small fixed wing UAV. The simulation results of longitudinal stability derivatives have been proved for the UAV system with the help of MATLAB/SIMULINK model. These methods can be used to convert the unstable conditions that cause by pole locations to stable conditions. And then the PID controller can be used to adjust the desired set point for ARF 60 UAV. Keywords – Modelling, Stability Analysis, Longitudinal Control, Fixed-wing UAV, MATLAB, SIMULINK model

Type : Research paper

Published : Volume-6,Issue-6


	\|		PDF	\|	Viewed - 80	\|	Published on 2018-08-13

Mar. 2025
Submitted Papers	:	80
Accepted Papers	:	10
Rejected Papers	:	70
Acc. Perc	:	12%
Issue Published	:	143
Paper Published	:	1781
No. of Authors	:	4956

Published : Volume-6,Issue-6

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