Rotorcraft trajectory tracking by supervised NLI control

A. Drouin, O. Lengerke, A. B. Ramos, F. Mora-Camino

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

2 Scopus citations

Abstract

The purpose of this communication is to present a new nonlinear control structure for trajectory tracking taking explicitly into account actuators saturation. Here trajectory tracking by a four rotor aircraft is considered. After introducing the flight dynamics equations for the four rotor aircraft, a trajectory tracking control structure based on a two layer non linear inverse approach is adopted and a supervision layer is introduced to take into account the possible actuators saturation.

Original languageEnglish
Title of host publicationInternational MultiConference of Engineers and Computer Scientists, IMECS 2012
PublisherNewswood Limited
Pages883-887
Number of pages5
ISBN (Print)9789881925190
StatePublished - 2012
Event2012 International MultiConference of Engineers and Computer Scientists, IMECS 2012 - Kowloon, Hong Kong
Duration: 14 Mar 201216 Mar 2012

Publication series

NameLecture Notes in Engineering and Computer Science
Volume2196
ISSN (Print)2078-0958

Conference

Conference2012 International MultiConference of Engineers and Computer Scientists, IMECS 2012
Country/TerritoryHong Kong
CityKowloon
Period14/03/1216/03/12

Keywords

  • Nonlinear inverse control
  • Rotorcraft
  • Saturation supervision
  • Trajectory tracking

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