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Comparative Study of PID Design Techniques for UAV 1-DOF Control via Genetic Algorithms

  • Universidad San Francisco de Quito

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

Abstract

This paper evaluates advanced PID control strategies applied to the 1-DOF Quanser Aero 2 system, a setup relevant to UAV pitch control during takeoff and landing. The classical PID serves as a benchmark against model-based approaches, including 2DOF PID, fractional-order PID, and nonlinear PID, as well as the model-free iPI controller. All controller parameters were optimized using genetic algorithms to ensure a fair comparison. Performance was assessed using standard metrics, including IAE, ISCO, overshoot, and settling time, under various reference and disturbance scenarios. Results highlight the strengths and trade-offs of each method, with a particular focus on their applicability in aerospace control tasks.

Original languageEnglish
Title of host publicationETCM 2025 - 9th Ecuador Technical Chapters Meeting
PublisherInstitute of Electrical and Electronics Engineers Inc.
ISBN (Electronic)9798331552640
DOIs
StatePublished - 2025
Event9th Ecuador Technical Chapters Meeting, ETCM 2025 - Quito, Ecuador
Duration: 21 Oct 202524 Oct 2025

Publication series

NameETCM 2025 - 9th Ecuador Technical Chapters Meeting

Conference

Conference9th Ecuador Technical Chapters Meeting, ETCM 2025
Country/TerritoryEcuador
CityQuito
Period21/10/2524/10/25

Keywords

  • 1-DOF
  • 2-DOF PID
  • FOPID
  • iPI
  • NPID
  • performance evaluation
  • PID control
  • Quanser Aero 2

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