Research on the flight control for an asymmetrical X-quadrotor

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Abstract

The paper presents an asymmetrical structure of X-quadrotor, which is different from the traditional quadrotor and is more complicated in the analysis of control forces and moments. A novel control method based on backstepping is applied in the attitude loop. And the compensation for perturbations of outer environment and noise of the measurements has been done. Then, various simulations are performed and the results show the system has a quick response with small overshoot and good dynamic characteristics. Finally, the experiments are implemented on the prototype. The flight test data has validated the robustness of the control algorithms.

Original languageEnglish
Title of host publicationMachinery Electronics and Control Engineering II
Pages399-402
Number of pages4
DOIs
Publication statusPublished - 2013
Event2012 2nd International Conference on Machinery Electronics and Control Engineering, ICMECE 2012 - Jinan, Shandong, China
Duration: 29 Dec 201230 Dec 2012

Publication series

NameApplied Mechanics and Materials
Volume313-314
ISSN (Print)1660-9336
ISSN (Electronic)1662-7482

Conference

Conference2012 2nd International Conference on Machinery Electronics and Control Engineering, ICMECE 2012
Country/TerritoryChina
CityJinan, Shandong
Period29/12/1230/12/12

Keywords

  • Asymmetrical structure
  • Backstepping
  • Quadrotor

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