Nonlinear forward path tracking controller for helicopter with slung load

Sami El-Ferik, Asim H. Syed, Hanafy M. Omar*, Mohamed A. Deriche

*Corresponding author for this work

Research output: Contribution to journalArticlepeer-review

37 Scopus citations

Abstract

In this paper, a tracking controller is designed for a helicopter with a slung load. The designed controller is nonlinear and is based on the backstopping method. First, we developed a comprehensive nonlinear mathematical model of the helicopter and designed a nonlinear backstepping controller to track the trajectory of the helicopter alone. Then, we developed a mathematical model of the slung load and integrated it with the helicopter system. In the next step, we designed an anti-swing delayed feedback controller to damp the load oscillation. This controller works independently of the nonlinear tracking controller. Moreover, its performance is optimized using the differential evolution (DE) technique. The simulation results show the effectiveness of the designed control system.

Original languageEnglish
Pages (from-to)602-608
Number of pages7
JournalAerospace Science and Technology
Volume69
DOIs
StatePublished - Oct 2017

Bibliographical note

Publisher Copyright:
© 2017 Elsevier Masson SAS

Keywords

  • Anti-swing controller
  • Backstepping nonlinear tracking control
  • Delayed feedback
  • Differential evolution
  • Helicopter slung load system

ASJC Scopus subject areas

  • Aerospace Engineering

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