Taxiing Control of Full-wing Solar-powered UAV by Using Differential Propeller Thrust

Ma Zhenyu, Z. H.U. Xiaoping, Zhou Zhou

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

Abstract

To solve the taxiing control problem under lack of nose wheel steering system and rudder, a control approach which uses differential propeller thrust to control taxiing is proposed, with full-wing solar-powered UAV (FSUAV) as the research model. This study gives the taxiing mathematical model of FSUAV and designs a taxiing controller based on linear active disturbance rejection control method (LADRC). Simulations are conducted to demonstrate the effectiveness and robustness of the designed controller and compare with PID controller.

Original languageEnglish
Title of host publication2018 IEEE CSAA Guidance, Navigation and Control Conference, CGNCC 2018
PublisherInstitute of Electrical and Electronics Engineers Inc.
ISBN (Electronic)9781538611715
DOIs
StatePublished - Aug 2018
Event2018 IEEE CSAA Guidance, Navigation and Control Conference, CGNCC 2018 - Xiamen, China
Duration: 10 Aug 201812 Aug 2018

Publication series

Name2018 IEEE CSAA Guidance, Navigation and Control Conference, CGNCC 2018

Conference

Conference2018 IEEE CSAA Guidance, Navigation and Control Conference, CGNCC 2018
Country/TerritoryChina
CityXiamen
Period10/08/1812/08/18

Keywords

  • differential propeller thrust
  • full-wing solar powered UAV
  • taxiing control

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