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
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