Flight dynamics and parametric modeling of a 2-DOF lab aircraft

Yasir Mahmood Khan, Sarvat M. Ahmad*, Mohsin Ali, Masroor Khan

*Corresponding author for this work

Research output: Contribution to journalArticlepeer-review

3 Scopus citations

Abstract

This paper presents two degrees-of-freedom (2-DOF) modeling of a lab aircraft extending corresponding author’s previous work on 1-DOF. The yaw motion is an additional DOF introduced along with the earlier work on pitch plane alone. The test-rig is designed, developed, instrumented, and interfaced with PC employing data acquisition card and real-time visualization software. Detailed mathematical models from first principles are developed incorporating important stability and control derivatives. The theoretical models are iteratively improved and validated through experimentation. The comparison reveals close agreement between math models and experimental ones. The developed high-fidelity models are to be employed for closed-loop control design and evaluation of system performance.

Original languageEnglish
Pages (from-to)2923-2931
Number of pages9
JournalProceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering
Volume233
Issue number8
DOIs
StatePublished - 1 Jun 2019
Externally publishedYes

Bibliographical note

Publisher Copyright:
© IMechE 2018.

Keywords

  • 2-DOF lab aircraft
  • Aerodynamic modeling
  • aircraft stability
  • unmanned air vehicles
  • wind tunnel

ASJC Scopus subject areas

  • Aerospace Engineering
  • Mechanical Engineering

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