Modeling and control of a quadrotor UAV with tilting propellers

Markus Ryll, Heinrich Bulthoff, Paolo Robuffo Giordano

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

109 Citations (Scopus)

Abstract

Standard quadrotor UAVs possess a limited mobility because of their inherent underactuation, i.e., availability of 4 independent control inputs (the 4 propeller spinning velocities) vs. the 6 dofs parameterizing the quadrotor position/ orientation in space. As a consequence, the quadrotor pose cannot track an arbitrary trajectory over time (e.g., it can hover on the spot only when horizontal). In this paper, we propose a novel actuation concept in which the quadrotor propellers are allowed to tilt about their axes w.r.t. the main quadrotor body. This introduces an additional set of 4 control inputs which provides full actuation to the quadrotor position/orientation. After deriving the dynamical model of the proposed quadrotor, we formally discuss its controllability properties and propose a nonlinear trajectory tracking controller based on dynamic feedback linearization techniques. The soundness of our approach is validated by means of simulation results.

Original languageEnglish
Title of host publicationProceedings - IEEE International Conference on Robotics and Automation
Pages4606-4613
Number of pages8
DOIs
Publication statusPublished - 2012 Aug 6

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ASJC Scopus subject areas

  • Software
  • Artificial Intelligence
  • Control and Systems Engineering
  • Electrical and Electronic Engineering

Cite this

Ryll, M., Bulthoff, H., & Giordano, P. R. (2012). Modeling and control of a quadrotor UAV with tilting propellers. In Proceedings - IEEE International Conference on Robotics and Automation (pp. 4606-4613). [6225129] https://doi.org/10.1109/ICRA.2012.6225129