DocumentCode :
3591708
Title :
Autonomous Control of a Quadcopter via Fuzzy Gain Scheduled PD Control
Author :
Sardar, Saad ; Kadri, Muhammad Bilal
Author_Institution :
Electr. & Power Eng. Dept., NUST, Karachi, Pakistan
fYear :
2014
Firstpage :
73
Lastpage :
78
Abstract :
This paper discusses the Intelligent Gain Scheduled PD technique to autonomously control the attitude of the Quad Copter. This paper would focus on two aspects of the autonomous quad-copter i.e. Attitude Control and Trajectory Following. The autonomous control of a quad-copter is a challenge due to its non-linear dynamics and environmental perturbations. The aim of the investigation is to study a Fuzzy Takagi-Sugeno method used to control the position and the yaw angle of the quad-copter and to compare the simulated results with the conventional PD Controller.
Keywords :
PD control; aircraft control; attitude control; fuzzy control; helicopters; nonlinear dynamical systems; perturbation techniques; scheduling; trajectory control; PD control; attitude control; autonomous control; environmental perturbation; fuzzy Takagi-Sugeno method; fuzzy gain scheduling; nonlinear dynamics; position control; quadcopter; trajectory following; yaw angle control; Adaptation models; Aerodynamics; Attitude control; Mathematical model; PD control; Rotors; Software packages; PD; Quadcopter; Takagi-Sugeno; fuzzy; gain-scheduling;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Frontiers of Information Technology (FIT), 2014 12th International Conference on
Print_ISBN :
978-1-4799-7504-4
Type :
conf
DOI :
10.1109/FIT.2014.23
Filename :
7118377
Link To Document :
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