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Chosen aspects of modeling and control of quadrotor platform

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

4 Citations (Scopus)

Abstract

This article is presenting the extended model of quadrotor platform together with a bespoken control system based on optimal approach. It highlights particular aspects of the derived model, such as inclusion of rotor gyroscopic effects and thrust generation based on momentum theory. The controller's behavior is tested by simulations. Comparisons with literature-available solutions to the problem of full quadrotor optimal control are made and important differences exposed. Conclusions are drawn and future work proposed.

Original languageEnglish
Title of host publication9th International Conference on Mathematical Problems in Engineering, Aerospace and Sciences, ICNPAA 2012
Pages1116-1122
Number of pages7
DOIs
Publication statusPublished - 2012
Event9th International Conference on Mathematical Problems in Engineering, Aerospace and Sciences, ICNPAA 2012 - Vienna, Austria
Duration: 10 Jul 201214 Jul 2012

Publication series

NameAIP Conference Proceedings
Volume1493
ISSN (Print)0094-243X
ISSN (Electronic)1551-7616

Conference

Conference9th International Conference on Mathematical Problems in Engineering, Aerospace and Sciences, ICNPAA 2012
Country/TerritoryAustria
CityVienna
Period10/07/1214/07/12

Keywords

  • Optimal Control
  • Quadrotor
  • Simulations
  • Unmanned Aerial Vehicles

ASJC Scopus subject areas

  • General Physics and Astronomy

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