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An attitude and orbit determination and control system for a small geostationary satellite

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

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Bibliographic Details
Main Author: Thopil, G. A.
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 Thopil, G. A.
author2 Steyn, W. H.
author_browse Steyn, W. H.
Thopil, G. A.
author_facet Steyn, W. H.
Thopil, G. A.
author_sort Thopil, G. A.
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:10019.1/2284
institution Stellenbosch University (South Africa)
language English
last_indexed 2026-06-10T12:41:19.170Z
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:10019.1/2284 An attitude and orbit determination and control system for a small geostationary satellite Thopil, G. A. Steyn, W. H. University of Stellenbosch. Faculty of Engineering. Dept. of Electrical and Electronic Engineering. Geostationary satellites Orbit control Attitude determination and control system Dissertations -- Electronic engineering Theses -- Electronic engineering Electrical and Electronic Engineering Thesis (MScEng (Electrical and Electronic Engineering))--University of Stellenbosch, 2006. An analysis of the attitude determination and control system required for a small geostationary satellite is performed in this thesis. A three axis quaternion feedback reaction wheel control system is the primary control system used to meet the stringent accuracy requirements. A momentum bias controller is also evaluated to provide redundancy and to extend actuator life. Momentum dumping is preformed by magnetic torque rods using a crossproduct controller. Performance of three axis thruster control is also evaluated. A full state Extended Kalman filter is used to determine attitude and body angular rates during normal operation whereas a Multiplicative Extended Kalman Filter is used during attitude manoeuvres. An analytical orbit control study is also performed to calculate the propellant required to perform station-keeping, for a specific sub-satellite location over a ten year period. Finally an investigation on the effects caused by thruster misalignment, on satellite attitude is also performed. 2008-08-04T09:56:48Z 2010-06-01T08:45:07Z 2008-08-04T09:56:48Z 2010-06-01T08:45:07Z 2006-12 Thesis http://hdl.handle.net/10019.1/2284 en University of Stellenbosch application/pdf Stellenbosch : University of Stellenbosch
spellingShingle Geostationary satellites
Orbit control
Attitude determination and control system
Dissertations -- Electronic engineering
Theses -- Electronic engineering
Electrical and Electronic Engineering
Thopil, G. A.
An attitude and orbit determination and control system for a small geostationary satellite
title An attitude and orbit determination and control system for a small geostationary satellite
title_full An attitude and orbit determination and control system for a small geostationary satellite
title_fullStr An attitude and orbit determination and control system for a small geostationary satellite
title_full_unstemmed An attitude and orbit determination and control system for a small geostationary satellite
title_short An attitude and orbit determination and control system for a small geostationary satellite
title_sort attitude and orbit determination and control system for a small geostationary satellite
topic Geostationary satellites
Orbit control
Attitude determination and control system
Dissertations -- Electronic engineering
Theses -- Electronic engineering
Electrical and Electronic Engineering
url http://hdl.handle.net/10019.1/2284
work_keys_str_mv AT thopilga anattitudeandorbitdeterminationandcontrolsystemforasmallgeostationarysatellite
AT thopilga attitudeandorbitdeterminationandcontrolsystemforasmallgeostationarysatellite