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Design, Modelling and Control of a Single Rotor UAV
2016 (English)Independent thesis Advanced level (professional degree), 20 credits / 30 HE creditsStudent thesis
Abstract [en]

In this thesis, a novel Vertical Take-Off and Landing (VTOL) Single Rotor Unmanned AerialVehicle (SR-UAV) will be presented. The SR-UAV’s design properties will be analysed indetail, with respect to technical novelties outlining the merits of such a conceptual approach.The system’s model will be mathematically formulated, while a cascaded P-PI and PID-basedcontrol structure will be utilized in extensive simulation trials for the preliminary evaluationof the SR-UAV’s attitude and translational performance. Further a prototype SR-UAV willbe presented with a corresponding experimental evaluation of the established control scheme.Finally analytic discussions on the obtained results, as well as on the current design limitationsand future research directions will also be depicted.

Place, publisher, year, edition, pages
2016.
Keyword [en]
Technology, UAV, Control, Robotics, modelling, design, single rotor, propeller, monocopter, helicopter, VTOL
Keyword [sv]
Teknik
Identifiers
URN: urn:nbn:se:ltu:diva-52220Local ID: 95aa487d-a496-4ee5-8eee-a46d14f69640OAI: oai:DiVA.org:ltu-52220DiVA: diva2:1025590
Subject / course
Student thesis, at least 30 credits
Educational program
Space Engineering, master's level
Examiners
Note
Validerat; 20160610 (global_studentproject_submitter)Available from: 2016-10-04 Created: 2016-10-04Bibliographically approved

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fulltext(32260 kB)228 downloads
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Carholt, Christoffer

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CiteExportLink to record
Permanent link

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Citation style
  • apa
  • ieee
  • modern-language-association-8th-edition
  • vancouver
  • Other style
More styles
Language
  • de-DE
  • en-GB
  • en-US
  • fi-FI
  • nn-NO
  • nn-NB
  • sv-SE
  • Other locale
More languages
Output format
  • html
  • text
  • asciidoc
  • rtf