Trajectory Tracking of a 2-DOF Helicopter System Using Canonical Normal Form

Soraya Bououden, Brahim Brahmi, Mohammad Habibur Rahman

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

2 Scopus citations

Abstract

This paper deals with canonical normal form approach for trajectory tracking control of a two degree-of-freedom helicopter system. The main objective is to stabilize beam of the helicopter with respect to pitch and yaw angles. Sufficient geometrical conditions are given for a class of nonlinear dynamical systems to transform the studied nonlinear systems into a triangular normal form and determine the flat outputs. Using this form two controllers are designed to control the position of the yaw and the pitch angles of the Helicopter. Simulation results are given to illustrate the effectiveness of the proposed control scheme.

Original languageEnglish
Title of host publication18th IEEE International Multi-Conference on Systems, Signals and Devices, SSD 2021
PublisherInstitute of Electrical and Electronics Engineers Inc.
Pages765-770
Number of pages6
ISBN (Electronic)9781665414937
DOIs
StatePublished - 22 Mar 2021
Externally publishedYes

Publication series

Name18th IEEE International Multi-Conference on Systems, Signals and Devices, SSD 2021

Bibliographical note

Publisher Copyright:
© 2021 IEEE.

Keywords

  • 2DOF
  • Flatness
  • Nonlinear systems
  • Normal Form

ASJC Scopus subject areas

  • Artificial Intelligence
  • Computer Networks and Communications
  • Computer Science Applications
  • Signal Processing
  • Electrical and Electronic Engineering

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