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Development of an attitude heading reference system for an airship

Thesis (MScEng (Electrical and Electronic Engineering))--University of Stellenbosch, 2006.

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Main Author: Bijker, Johan
Other Authors: Steyn, W. H.
Format: Thesis
Language:English
Published: Stellenbosch : University of Stellenbosch 2008
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access_status_str Open Access
author Bijker, Johan
author2 Steyn, W. H.
author_browse Bijker, Johan
Steyn, W. H.
author_facet Steyn, W. H.
Bijker, Johan
author_sort Bijker, Johan
collection Thesis
dc_rights_str_mv University of Stellenbosch
description Thesis (MScEng (Electrical and Electronic Engineering))--University of Stellenbosch, 2006.
format Thesis
id oai:scholar.sun.ac.za:10019.1/1551
institution Stellenbosch University (South Africa)
language English
last_indexed 2026-06-10T12:44:12.049Z
license_str Other — see source repository
provenance_str_mv Harvested via OAI-PMH from SUNScholar — Stellenbosch University Repository
publishDate 2008
publishDateRange 2008
publishDateSort 2008
publisher Stellenbosch : University of Stellenbosch
publisherStr Stellenbosch : University of Stellenbosch
record_format dspace
source_str SUNScholar — Stellenbosch University Repository
spelling oai:scholar.sun.ac.za:10019.1/1551 Development of an attitude heading reference system for an airship Bijker, Johan Steyn, W. H. University of Stellenbosch. Faculty of Engineering. Dept. of Electrical and Electronic Engineering. Theses -- Electronic engineering Dissertations -- Electronic engineering Airships Flight control Guidance systems (Flight) Drone aircraft Thesis (MScEng (Electrical and Electronic Engineering))--University of Stellenbosch, 2006. A real time attitude and heading reference system (AHRS) was successfully implemented for use on an airship. The AHRS was tested on board a small airship (blimp) with real data supplied from the inertial measurement unit and GPS receiver. The inertial measurement unit was built with lower grade sensors, resulting in significant reductions in component cost. To ensure accurate navigation results, the high rate inertial measurements were complemented with low rate GPS velocity and position updates in an extended Kalman filter configuration. A study was made of various Kalman filter configurations, especially the possibility of splitting a big Kalman filter into smaller Kalman filters. It was found that the best trade-off between accuracy and processing power was achieved by having two smaller Kalman filters running in sequence. The first extended Kalman filter estimates the attitude of the airship, while the second extended Kalman filter estimates the velocity and position of the airship. The two smaller Kalman filters were implemented on an onboard computer to provide real time estimates of the attitude, velocity and position of the airship. 2008-01-23T08:08:32Z 2010-06-01T08:27:09Z 2008-01-23T08:08:32Z 2010-06-01T08:27:09Z 2006-12 Thesis http://hdl.handle.net/10019.1/1551 en University of Stellenbosch 1880280 bytes application/pdf application/pdf Stellenbosch : University of Stellenbosch
spellingShingle Theses -- Electronic engineering
Dissertations -- Electronic engineering
Airships
Flight control
Guidance systems (Flight)
Drone aircraft
Bijker, Johan
Development of an attitude heading reference system for an airship
title Development of an attitude heading reference system for an airship
title_full Development of an attitude heading reference system for an airship
title_fullStr Development of an attitude heading reference system for an airship
title_full_unstemmed Development of an attitude heading reference system for an airship
title_short Development of an attitude heading reference system for an airship
title_sort development of an attitude heading reference system for an airship
topic Theses -- Electronic engineering
Dissertations -- Electronic engineering
Airships
Flight control
Guidance systems (Flight)
Drone aircraft
url http://hdl.handle.net/10019.1/1551
work_keys_str_mv AT bijkerjohan developmentofanattitudeheadingreferencesystemforanairship