Published February 2013 | Version public
Journal Article

Introduction to Feedback Control of Underactuated VTOL Vehicles

  • 1. ROR icon Sorbonne University
  • 2. ROR icon Laboratoire d'Informatique, Signaux et Systèmes de Sophia Antipolis
  • 3. ROR icon Research Centre Inria Sophia Antipolis - Méditerranée

Abstract

This article is an introduction to feedback control design for a family of robotic aerial vehicles with vertical take-off and landing (VTOL) capabilities such as quadrotors, ducted-fan tail-sitters, and helicopters. Potential applications for such devices, like surveillance, monitoring, or mapping, are varied and numerous. For these applications to emerge, motion control algorithms that guarantee a good amount of robustness against state measurement/ estimation errors and unmodeled dynamics like, for example, aerodynamic perturbations, are needed. The feedback control methods considered here range from basic linear control schemes to more elaborate nonlinear control solutions. The modeling of the dynamics of these systems is first recalled and discussed. Then several control algorithms are presented and commented upon in relation to implementation issues and various operating modes encountered in practice, from teleoperated to fully autonomous flight. Particular attention is paid to the incorporation of integral-like control actions, often overlooked in nonlinear control studies despite their practical importance to render the control performance more robust with respect to unmodeled or poorly estimated additive perturbations.

Additional Information

© 2013 IEEE. Date of Current Version: 18 January 2013. Issue Date: Feb. 2013. This work has been supported by the Chaire d'excellence en robotique RTE-UPMC

Additional details

Identifiers

Eprint ID
37113
DOI
10.1109/MCS.2012.2225931
Resolver ID
CaltechAUTHORS:20130225-111724208

Related works

Funding

Chaire d'excellence en robotique RTE-UPMC

Dates

Created
2013-02-25
Created from EPrint's datestamp field
Updated
2021-11-09
Created from EPrint's last_modified field

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INSPEC Accession Number
Other Numbering System Identifier
13244918