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Fractional order controller for pitch loop control of a VTOL UAV

TitleFractional order controller for pitch loop control of a VTOL UAV
Publication TypeConference Paper
Year of Publication2013
AuthorsHan, J, Di, L, Coopmans, C, Chen, YQ
Conference Name2013 International Conference on Unmanned Aircraft Systems (ICUAS)
Date Publishedmay
PublisherIEEE
ISBN Number978-1-4799-0817-2
KeywordsARX model, Attitude control, auto-regressive with exogenous input model, autonomous aerial vehicles, autoregressive processes, Control systems, delays, disturbance rejection, Educational institutions, first-order plus time delay model, FOPTD model, fractional order controller, general integer order proportional integral deriva, integer order PI controller, Mathematical model, MZN tuning rule, PI control, PID controller, pitch loop control, robust control, Robustness, three-term control, Tuning, Unmanned aerial vehicles, vertical takeoff and landing, VTOL UAV, Ziegler-Nichols tuning rule
Abstract

As the fundamental tuning step for vertical takeoff and landing (VTOL) unmanned aerial vehicles (UAVs), pitch loop control has significant impact on the flight. In this paper, an auto-regressive with exogenous input (ARX) model is acquired and converted to a first-order plus time delay (FOPTD) model for the pitch loop of a VTOL UAV. Based on the FOPTD model, a fractional order [proportional integral] (FO[PI]) controller is designed. An integer order PI controller based on the modified Ziegler-Nichols (MZNs) tuning rule and a general integer order proportional integral derivative (PID) controller are also designed for comparison following three design specifications. Simulation results have shown that the proposed fractional order controller outperforms both the MZNs PI controller and the integer order PID controller in terms of robustness and disturbance rejection.

URLhttp://ieeexplore.ieee.org/lpdocs/epic03/wrapper.htm?arnumber=6564739
DOI10.1109/ICUAS.2013.6564739

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