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Control and formation flying for the quadrotor UAV

  • Beihang University

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

Abstract

In this paper, control and formation flying for the mini quadrotor UAV are studied. First, the quadrotor UAV is modeled and its simplified mathematical model is given. And then using the traditional PID method in all the designed controller channels, each channel is given in the simulation under different excitation curve. Next the formation problem of the mini quadrotor UAV is analyzed with establishing the dynamic equation of a wingman and the relevant simulation curve is given at last.

Original languageEnglish
Title of host publication2011 International Conference on Photonics, 3D-Imaging, and Visualization
DOIs
StatePublished - 2011
Event2011 International Conference on Photonics, 3D-Imaging, and Visualization - Guangzhou, China
Duration: 30 Oct 201131 Oct 2011

Publication series

NameProceedings of SPIE - The International Society for Optical Engineering
Volume8205
ISSN (Print)0277-786X

Conference

Conference2011 International Conference on Photonics, 3D-Imaging, and Visualization
Country/TerritoryChina
CityGuangzhou
Period30/10/1131/10/11

Keywords

  • Mini quadrotor UAV
  • PID control
  • formation flying
  • wingman

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