Global Chartwise Feedback Linearization of the Quadcopter with a Thrust Positivity Preserving Dynamic Extension

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Abstract

We propose a new dynamic extension of the thrust variable in the quadcopter dynamics that preserves the positive sign of the thrust. This extension not only eliminates the positive sign constraint on the thrust variable, but also leads to global chartwise feedback linearization of the quadcopter dynamics. For the latter, an atlas is first constructed on the entire state space of the quadcopter and then the dynamically extended quadcopter system is transformed to a 14-dimensional linear controllable system on each chart in the atlas. Based on the chartwise dynamic feedback linearization, a global tracking strategy is proposed for the quadcopter and its excellent performance is demonstrated with a simulation.

Original languageEnglish
Article number7879259
Pages (from-to)4747-4752
Number of pages6
JournalIEEE Transactions on Automatic Control
Volume62
Issue number9
DOIs
StatePublished - Sep 2017

Bibliographical note

Publisher Copyright:
© 1963-2012 IEEE.

Keywords

  • Atlas
  • differential flatness
  • dynamic feedback linearization
  • global tracking
  • quadcopter
  • quadrocopter
  • quadrotor

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