Control of an octa-copter from modeling to experiments

  • Hyeonbeom Lee
  • , Suseong Kim
  • , Hyon Lim
  • , H. Jin Kim
  • , Daewon Lee

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Abstract

This paper presents modeling and stabilization of an octa-copter which can carry heavier payload than a quadrotor. We explain the method for obtaining desired motor speed of the octa-copter using a simple assumption. By employing adaptive sliding mode control, the uncertainty for the octa-rotor such as modeling error and unknown ground effects is resolved. Experimental results from hovering flight tests are validated using the flight tests with vicon system.

Original languageEnglish (US)
Title of host publication2013 44th International Symposium on Robotics, ISR 2013
DOIs
StatePublished - 2013
Externally publishedYes
Event2013 44th IEEE International Symposium on Robotics, ISR 2013 - Seoul, Korea, Republic of
Duration: Oct 24 2013Oct 26 2013

Publication series

Name2013 44th International Symposium on Robotics, ISR 2013

Conference

Conference2013 44th IEEE International Symposium on Robotics, ISR 2013
Country/TerritoryKorea, Republic of
CitySeoul
Period10/24/1310/26/13

All Science Journal Classification (ASJC) codes

  • Artificial Intelligence
  • Human-Computer Interaction

Keywords

  • heavy lifting UAVs
  • Octa-rotor
  • quadrotor
  • sliding mode control
  • UAVs

Fingerprint

Dive into the research topics of 'Control of an octa-copter from modeling to experiments'. Together they form a unique fingerprint.

Cite this