A Study of the Interaction of Proportional-Integral- Derivative (PID) Control in a Quadcopter Unmanned Aerial Vehicle (UAV) Using Design of Experiment

College

Gokongwei College of Engineering

Department/Unit

Electronics And Communications Engg

Document Type

Conference Proceeding

Source Title

2019 IEEE 11th International Conference on Humanoid, Nanotechnology, Information Technology, Communication and Control, Environment, and Management, HNICEM 2019

Publication Date

11-1-2019

Abstract

© 2019 IEEE. UAV applications are dependent on the stability of flight it can perform. Visually, poor flight stability appears to be having a shaking or oscillating movement that is not desirable, while good flight stability lacks this kind of effect. It is important to be able to tune the control system so that the flight performance of the UAV will be steady and free from oscillating motion. PID control is one of the commonly used control schemes to create a stable flight for UAVs. In this paper, the interaction of the PID values on the stability of the flight is investigated using Design of Experiment. A 2K Factorial Design is used as the experimental design to observe which factors and interactions, or both, significantly affect the stability of the quadcopter UAV. Using Analysis of Variance (ANOVA), the result of the experiment showed that the interaction of PI and PD values are significant in minimizing the error of the flight stability of the tested UAV system setup.

html

Digitial Object Identifier (DOI)

10.1109/HNICEM48295.2019.9072806

Upload File

wf_yes

This document is currently not available here.

Share

COinS