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The development of Sun and Nadir sensors for a solar sail CubeSat

Thesis (MScEng (Electrical and Electronic Engineering))--University of Stellenbosch, 2011.

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Bibliographic Details
Main Author: Loubser, Hanco Evert
Other Authors: Steyn, W. H.
Format: Thesis
Language:en_ZA
Published: Stellenbosch : University of Stellenbosch 2011
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access_status_str Open Access
author Loubser, Hanco Evert
author2 Steyn, W. H.
author_browse Loubser, Hanco Evert
Steyn, W. H.
author_facet Steyn, W. H.
Loubser, Hanco Evert
author_sort Loubser, Hanco Evert
collection Thesis
dc_rights_str_mv University of Stellenbosch
description Thesis (MScEng (Electrical and Electronic Engineering))--University of Stellenbosch, 2011.
format Thesis
id oai:scholar.sun.ac.za:10019.1/6748
institution Stellenbosch University (South Africa)
language en_ZA
last_indexed 2026-06-10T12:47:14.419Z
license_str Other — see source repository
provenance_str_mv Harvested via OAI-PMH from SUNScholar — Stellenbosch University Repository
publishDate 2011
publishDateRange 2011
publishDateSort 2011
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:10019.1/6748 The development of Sun and Nadir sensors for a solar sail CubeSat Loubser, Hanco Evert Steyn, W. H. University of Stellenbosch. Faculty of Engineering. Dept. of Electrical and Electronic Engineering. Attitude Determination Control System (ADCS) CubeSat Picosatellite Miniaturised sensors 3-axis orientation Dissertations -- Electronic engineering Theses -- Electronic engineering Solar sails Artificial satellites Thesis (MScEng (Electrical and Electronic Engineering))--University of Stellenbosch, 2011. ENGLISH ABSTRACT: This thesis describes the development of attitude sensors required for the Attitude Determination and Control System (ADCS) for a Cubesat. The aim is to find the most suitable sensors for use on a small picosatellite by implementing miniaturised sensors with available commercial-off-the-shelf (COTS) technology. Specifically, the algorithms, hardware prototypes, software and filters required to create accurate sensors to determine the 3-axis orientation of a CubeSat are discussed. AFRIKAANSE OPSOMMING: Hierdie tesis beskryf die ontwikkeling van oriëntasiesensors wat benodig word vir die oriëntasiebepaling en -beheerstelsel (Engels: ADCS) van ’n CubeSat. Die doelwit is om sensors te vind wat die geskikste is om in ’n klein picosatelliet te gebruik, deur miniatuursensors met kommersiële maklik verkrygbare tegnologie (Engels: COTS technology) te implementeer. Daar word in die bespreking veral aandag geskenk aan die algoritmes, hardewareprototipes, programmatuur en filters wat benodig word om akkurate sensors te skep wat op hul beurt 3-as oriëntasie van die CubeSat kan bepaal. 2011-02-28T10:43:49Z 2011-03-14T08:37:33Z 2011-02-28T10:43:49Z 2011-03-14T08:37:33Z 2011-03 Thesis http://hdl.handle.net/10019.1/6748 en_ZA University of Stellenbosch 105 p. : ill. application/pdf Stellenbosch : University of Stellenbosch
spellingShingle Attitude Determination Control System (ADCS)
CubeSat
Picosatellite
Miniaturised sensors
3-axis orientation
Dissertations -- Electronic engineering
Theses -- Electronic engineering
Solar sails
Artificial satellites
Loubser, Hanco Evert
The development of Sun and Nadir sensors for a solar sail CubeSat
title The development of Sun and Nadir sensors for a solar sail CubeSat
title_full The development of Sun and Nadir sensors for a solar sail CubeSat
title_fullStr The development of Sun and Nadir sensors for a solar sail CubeSat
title_full_unstemmed The development of Sun and Nadir sensors for a solar sail CubeSat
title_short The development of Sun and Nadir sensors for a solar sail CubeSat
title_sort development of sun and nadir sensors for a solar sail cubesat
topic Attitude Determination Control System (ADCS)
CubeSat
Picosatellite
Miniaturised sensors
3-axis orientation
Dissertations -- Electronic engineering
Theses -- Electronic engineering
Solar sails
Artificial satellites
url http://hdl.handle.net/10019.1/6748
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