Skip to main navigation Skip to search Skip to main content

L1 fault tolerant adaptive control of a hexacopter with control degradation

  • Technical University of Munich

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

22 Scopus citations

Abstract

In this paper we present a nonlinear control framework for the attitude of a hexacopter system, which is able to cope with motor degradation. Approximate model inversion transforms the plant into an equivalent linear form. A linear error controller enables tracking of a designer chosen reference model. The control framework is augmented by an L1 adaptive controller, in order to cope with uncertainties. Due to the nature of the L1 controller, performance and robustness are decoupled, which allows for a fast and reliable compensation of faults. We present a condition on the control allocation in order to achieve attitude stabilization during hover. The performance of the control architecture is corroborated in numerical simulation using a high fidelity simulation model of a hexacopter system. After that flight test results with motor degradation are presented.

Original languageEnglish
Title of host publication2015 IEEE Conference on Control and Applications, CCA 2015 - Proceedings
PublisherInstitute of Electrical and Electronics Engineers Inc.
Pages750-755
Number of pages6
ISBN (Electronic)9781479977871
DOIs
StatePublished - 4 Nov 2015
EventIEEE Conference on Control and Applications, CCA 2015 - Sydney, Australia
Duration: 21 Sep 201523 Sep 2015

Publication series

Name2015 IEEE Conference on Control and Applications, CCA 2015 - Proceedings

Conference

ConferenceIEEE Conference on Control and Applications, CCA 2015
Country/TerritoryAustralia
CitySydney
Period21/09/1523/09/15

Fingerprint

Dive into the research topics of 'L1 fault tolerant adaptive control of a hexacopter with control degradation'. Together they form a unique fingerprint.

Cite this