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Geometric nonlinear PID control of a quadrotor UAV on SE(3)

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

Abstract

Nonlinear PID control systems for a quadrotor UAV are proposed to follow an attitude tracking command and a position tracking command. The control systems are developed directly on the special Euclidean group to avoid singularities of minimal attitude representations or ambiguity of quaternions. A new form of integral control terms is proposed to guarantee almost global asymptotic stability when there exist uncertainties in the quadrotor dynamics. A rigorous mathematical proof is given. Numerical example illustrating a complex maneuver, and a preliminary experimental result are provided.

Original languageEnglish (US)
Title of host publication2013 European Control Conference, ECC 2013
PublisherIEEE Computer Society
Pages3845-3850
Number of pages6
ISBN (Print)9783033039629
DOIs
StatePublished - 2013
Externally publishedYes
Event2013 12th European Control Conference, ECC 2013 - Zurich, Switzerland
Duration: Jul 17 2013Jul 19 2013

Publication series

Name2013 European Control Conference, ECC 2013

Conference

Conference2013 12th European Control Conference, ECC 2013
Country/TerritorySwitzerland
CityZurich
Period7/17/137/19/13

All Science Journal Classification (ASJC) codes

  • Control and Systems Engineering

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