Research on the attitude control of unmanned multi-ducted-fan flying vehicle

Yue Ma, Wanming Chen, Lu Lin, Yu Wang

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

Abstract

The unmanned multi-ducted-fan flying vehicle is a kind of novel multi-purpose platform for future transportation. In this paper, flight dynamics model is established based on aerodynamics principles and rigid body dynamics theory. To make the controller of the multi-ducted fan flying vehicle more robust, a double closed loop PID controller is put forward with non-smooth parameters optimization method. Numerical simulation and field the experimental results demonstrate that the PID controller has good performance on the inner-loop attitude control in forward flight.

Original languageEnglish
Title of host publication2017 21st International Conference on System Theory, Control and Computing, ICSTCC 2017
EditorsMarius Kloetzer, Lavinia Ferariu
PublisherInstitute of Electrical and Electronics Engineers Inc.
Pages321-327
Number of pages7
ISBN (Electronic)9781538638422
DOIs
Publication statusPublished - 13 Nov 2017
Event21st International Conference on System Theory, Control and Computing, ICSTCC 2017 - Sinaia, Romania
Duration: 19 Oct 201721 Oct 2017

Publication series

Name2017 21st International Conference on System Theory, Control and Computing, ICSTCC 2017

Conference

Conference21st International Conference on System Theory, Control and Computing, ICSTCC 2017
Country/TerritoryRomania
CitySinaia
Period19/10/1721/10/17

Keywords

  • double closed loop PID
  • multi-ducted-fan flying vehicle
  • non-smooth optimization

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