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Strategies for the control of a satellite with thruster misalignment

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

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Bibliographic Details
Main Author: Van Daalen, Corne E.
Other Authors: Treurnicht, J.
Format: Thesis
Language:en_ZA
Published: Stellenbosch : University of Stellenbosch 2006
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access_status_str Open Access
author Van Daalen, Corne E.
author2 Treurnicht, J.
author_browse Treurnicht, J.
Van Daalen, Corne E.
author_facet Treurnicht, J.
Van Daalen, Corne E.
author_sort Van Daalen, Corne E.
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:10019.1/2306
institution Stellenbosch University (South Africa)
language en_ZA
last_indexed 2026-06-10T12:41:16.700Z
license_str Other — see source repository
provenance_str_mv Harvested via OAI-PMH from SUNScholar — Stellenbosch University Repository
publishDate 2006
publishDateRange 2006
publishDateSort 2006
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:10019.1/2306 Strategies for the control of a satellite with thruster misalignment Van Daalen, Corne E. Treurnicht, J. University of Stellenbosch. Faculty of Engineering. Dept. of Electrical and Electronic Engineering. Artificial satellites -- Control systems Artificial satellites -- Propulsion systems Dissertations -- Electronic engineering Theses -- Electronic engineering Electrical and Electronic Engineering Thesis (MScEng (Electrical and Electronic Engineering))--University of Stellenbosch, 2006. This project investigates two problems related to satellites that contain cold gas thrusters and reaction wheels. The first problem concerns the estimation of the thruster force response to a pulse command. An optimal data integration method is developed and implemented to estimate the thruster force output from a number of noisy sensors. The second problem occurs when the output force vector of a thruster mounted on a satellite is misaligned with the centre of mass with the satellite. As a result a disturbance torque is generated on the satellite during thruster operation. 2006-11-16T06:27:45Z 2010-06-01T08:45:39Z 2006-11-16T06:27:45Z 2010-06-01T08:45:39Z 2006-03 Thesis http://hdl.handle.net/10019.1/2306 en_ZA University of Stellenbosch 2339796 bytes application/pdf application/pdf Stellenbosch : University of Stellenbosch
spellingShingle Artificial satellites -- Control systems
Artificial satellites -- Propulsion systems
Dissertations -- Electronic engineering
Theses -- Electronic engineering
Electrical and Electronic Engineering
Van Daalen, Corne E.
Strategies for the control of a satellite with thruster misalignment
title Strategies for the control of a satellite with thruster misalignment
title_full Strategies for the control of a satellite with thruster misalignment
title_fullStr Strategies for the control of a satellite with thruster misalignment
title_full_unstemmed Strategies for the control of a satellite with thruster misalignment
title_short Strategies for the control of a satellite with thruster misalignment
title_sort strategies for the control of a satellite with thruster misalignment
topic Artificial satellites -- Control systems
Artificial satellites -- Propulsion systems
Dissertations -- Electronic engineering
Theses -- Electronic engineering
Electrical and Electronic Engineering
url http://hdl.handle.net/10019.1/2306
work_keys_str_mv AT vandaalencornee strategiesforthecontrolofasatellitewiththrustermisalignment