Change search
ReferencesLink to record
Permanent link

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

Open Access in DiVA

fulltext(1604 kB)4 downloads
File information
File name FULLTEXT01.pdfFile size 1604 kBChecksum SHA-512
Type fulltextMimetype application/pdf

Search outside of DiVA

GoogleGoogle Scholar
Total: 4 downloads
The number of downloads is the sum of all downloads of full texts. It may include eg previous versions that are now no longer available

Total: 1 hits
ReferencesLink to record
Permanent link

Direct link