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Estimation of angular positions of a UAV from inertial measurements
2009 (English)Independent thesis Advanced level (degree of Master (Two Years)), 20 credits / 30 HE creditsStudent thesis
Abstract [en]

This project consists of the design and development of a navigational unit for a UAV (Unmanned Air Vehicle). The purpose is to design from scratch a device that would use three accelerometers, three gyroscopes, a magnetometer and a GPS to provide an estimation of the angular position of the UAV. The tasks involved selecting appropriate sensors, designing a circuit board, assembling the board, connecting the sensors and testing them. A mathematical model of the plane dynamics was also provided to increase the accuracy of the measurement. One extra task was to translate this model, provided in MatLab, into C code.

Place, publisher, year, edition, pages
2009.
Keyword [en]
Technology, GPS, Inertial Sensors, Gyros, Accelerometers, Magnetometers, ARM processor
Keyword [sv]
Teknik
Identifiers
URN: urn:nbn:se:ltu:diva-42098ISRN: LTU-PB-EX--09/014--SELocal ID: 0275bb40-103d-438f-9e1e-cd9fea9c43cbOAI: oai:DiVA.org:ltu-42098DiVA, id: diva2:1015314
Subject / course
Student thesis, at least 30 credits
Educational program
Space Engineering, master's level
Examiners
Note
Validerat; 20101217 (root)Available from: 2016-10-04 Created: 2016-10-04Bibliographically approved

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Type fulltextMimetype application/pdf

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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