UAV path following based on BLADRC and inverse dynamic guidance approach

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

Abstract

In this paper, a three-dimensional UAV path following control system accounting for wind disturbance is designed to realize the mission that UAV can fly along the given waypoints. The system is divided into angular rate loop, angle loop, flight path loop and position loop. For the angular rate loop and the angle loop, they are based on back-stepping linear active disturbance rejection control (BLADRC). For the flight path loop, it is based on a novel maneuver generator (MG) with BLADRC and inverse dynamic method. For the position loop, it is based on the inverse dynamic guidance law. By utilizing the proposed control system, UAV can fly along the given waypoints and converge to straight-line paths between waypoints. The path can be adjusted online.

Original languageEnglish
Title of host publication2017 Asian Control Conference, ASCC 2017
PublisherInstitute of Electrical and Electronics Engineers Inc.
Pages400-405
Number of pages6
ISBN (Electronic)9781509015733
DOIs
StatePublished - 7 Feb 2018
Event2017 11th Asian Control Conference, ASCC 2017 - Gold Coast, Australia
Duration: 17 Dec 201720 Dec 2017

Publication series

Name2017 Asian Control Conference, ASCC 2017
Volume2018-January

Conference

Conference2017 11th Asian Control Conference, ASCC 2017
Country/TerritoryAustralia
CityGold Coast
Period17/12/1720/12/17

Keywords

  • UAV
  • back-stepping active disturbance rejection control
  • inverse dynamic method
  • maneuver generator
  • three-dimensional path following
  • wind disturbance

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