4.6 Article

Roll-channel fractional order controller design for a small fixed-wing unmanned aerial vehicle

Journal

CONTROL ENGINEERING PRACTICE
Volume 18, Issue 7, Pages 761-772

Publisher

PERGAMON-ELSEVIER SCIENCE LTD
DOI: 10.1016/j.conengprac.2010.02.003

Keywords

Fractional order controller; Unmanned aerial vehicle; Flight control; PID controller

Funding

  1. Utah Water Research Laboratory (UWRL)
  2. China Scholarship Council (CSC)
  3. Direct For Computer & Info Scie & Enginr
  4. Division Of Computer and Network Systems [0851709] Funding Source: National Science Foundation

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Low-cost small unmanned aerial vehicles (UAVs) attracted researchers and developers around the world for use in both military and civilian applications. However, there are challenges in designing stable and robust flight controllers that handle the UAV model and environmental uncertainties. This paper focuses on the design and implementation of a roll-channel fractional order proportional integral (PI lambda) flight controller for a small fixed-wing UAV. Time domain system identification methods are used to obtain a simple auto-regressive with exogenous input (ARX) model of the UAV roll-channel. A new fractional order PI controller design method is introduced based on the identified simple model. The fractional order PI lambda controller outperforms the optimized traditional integer order proportional integral derivative (PID) controller due to the fractional order introduced as a design parameter. The simulation results show the effectiveness of the proposed controller design strategy and the robustness of fractional order controller under conditions of wind gusts and payload variations. Further real flight test results are also provided to show the advantages of the proposed PI lambda controller. (c) 2010 Elsevier Ltd. All rights reserved.

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