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Real-time flight control design for a spherical blimp

  • Arturo Rojas-Moreno
  • , Freddy Santos-Rodriguez
  • , Noel Curinaupa-Cespedes

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

1 Scopus citations

Abstract

This paper develops a real-time software written in LabVIEW code to test a novel flight control strategy for a spherical blimp. Such a blimp will have an spherical hull filled with helium. Four tetrahedrally-arranged driving units (DU) were designed and constructed, with each DU having a thruster with propeller with the ability to rotate, due to the action of a DC servomotor. Such DU will be mounted on the blimp for locomotion. The mechanical design is aimed to make the blimp near NBP (Neutral Buoyancy Position). Starting from any NBP, the proposed flight logic strategy permits the blimp to move in any direction: up, down, right, left, forward and backward.

Original languageEnglish
Title of host publicationProceedings of the 2016 IEEE 23rd International Congress on Electronics, Electrical Engineering and Computing, INTERCON 2016
PublisherInstitute of Electrical and Electronics Engineers Inc.
ISBN (Electronic)9781509013401
DOIs
StatePublished - 12 Jan 2017
Event23rd IEEE International Congress on Electronics, Electrical Engineering and Computing, INTERCON 2016 - Piura, Peru
Duration: 2 Aug 20165 Aug 2016

Publication series

NameProceedings of the 2016 IEEE 23rd International Congress on Electronics, Electrical Engineering and Computing, INTERCON 2016

Conference

Conference23rd IEEE International Congress on Electronics, Electrical Engineering and Computing, INTERCON 2016
Country/TerritoryPeru
CityPiura
Period2/08/165/08/16

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