Modeling and PD control of a quadrotor VTOL vehicle

Bora Erginer, Erdinç Altuǧ

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

248 Citations (Scopus)

Abstract

In this paper, we present a model of a four rotor vertical take-off and landing (VTOL) unmanned air vehicle known as quadrotor aircraft. And we explained its control architecture including vision based control. Quadrotors have generated considerable interest in both the control community due to their complex dynamics and military because of their advantages over regular air vehicles. The proposed dynamical model which comprises gyroscopic effects and its control strategies can be source for future works.

Original languageEnglish
Title of host publicationProceedings of the 2007 IEEE Intelligent Vehicles Symposium, IV 2007
PublisherInstitute of Electrical and Electronics Engineers Inc.
Pages894-899
Number of pages6
ISBN (Print)1424410681, 9781424410682
DOIs
Publication statusPublished - 2007
Event2007 IEEE Intelligent Vehicles Symposium, IV 2007 - Istanbul, Turkey
Duration: 13 Jun 200715 Jun 2007

Publication series

NameIEEE Intelligent Vehicles Symposium, Proceedings

Conference

Conference2007 IEEE Intelligent Vehicles Symposium, IV 2007
Country/TerritoryTurkey
CityIstanbul
Period13/06/0715/06/07

Keywords

  • Aircraft control
  • Modeling
  • Quadrotor
  • Unmanned Aerial Vehicle (UAV)

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