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The instrumentation and initial analysis of the short-term control and stability derivatives of an ASK-I3 glider

Thesis (MScEng (Electrical and Electronic Engineering))--University of Stellenbosch, 2004. 220 leaves single printed pages ,preliminary pages i-xiv and numberd pages 1-188.Includes bibliography.list of figures and used a Hp Scanjet 8250 Scanner to pdf format (OCR),

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Bibliographic Details
Main Author: Browne, Keith R.J.
Other Authors: Milne, G. W.
Format: Thesis
Language:English
Published: Stellenbosch : University of Stellenbosch 2010
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access_status_str Open Access
author Browne, Keith R.J.
author2 Milne, G. W.
author_browse Browne, Keith R.J.
Milne, G. W.
author_facet Milne, G. W.
Browne, Keith R.J.
author_sort Browne, Keith R.J.
collection Thesis
dc_rights_str_mv University of Stellenbosch
description Thesis (MScEng (Electrical and Electronic Engineering))--University of Stellenbosch, 2004. 220 leaves single printed pages ,preliminary pages i-xiv and numberd pages 1-188.Includes bibliography.list of figures and used a Hp Scanjet 8250 Scanner to pdf format (OCR),
format Thesis
id oai:scholar.sun.ac.za:10019.1/3631
institution Stellenbosch University (South Africa)
language English
last_indexed 2026-06-10T12:42:50.594Z
license_str Other — see source repository
provenance_str_mv Harvested via OAI-PMH from SUNScholar — Stellenbosch University Repository
publishDate 2010
publishDateRange 2010
publishDateSort 2010
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:10019.1/3631 The instrumentation and initial analysis of the short-term control and stability derivatives of an ASK-I3 glider Browne, Keith R.J. Milne, G. W. University of Stellenbosch. Faculty of Engineering. Dept. of Electrical and Electronic Engineering. Control surface deflections MMLE3 implementation Dissertations -- Electronic engineering Theses -- Electronic engineering Gliders (Aeronautics) Airplanes -- Flight testing Flight control Thesis (MScEng (Electrical and Electronic Engineering))--University of Stellenbosch, 2004. 220 leaves single printed pages ,preliminary pages i-xiv and numberd pages 1-188.Includes bibliography.list of figures and used a Hp Scanjet 8250 Scanner to pdf format (OCR), ENGLISH ABSTRACT: This thesis describes the process followed to determine the short-term control and stability derivatives of an ASK-13 glider (ZS-GHB). The short-term control and stability derivatives are obtained by parameter estimation done using data recorded in flight. The algorithm used is the MMLE3 implementation of a maximum likelihood estimator. To collect the flight data sensors were installed in the ZS-GHB. Sensors measuring the control surface deflections, translation acceleration, angular rates and the dynamic and static pressure are needed to provide enough data for the estimation. To estimate accurate derivatives specific manoeuvres were flown by the pilot, to ensure that all the modes of the glider were stimulated. The results reveal that the control and stability derivatives estimated from the flight data are not very accurate but are still suitable to be used in simulating the glider's motion. AFRIKAANSE OPSOMMING: Hierdie tesis beskryf die proses wat gebruik is om die kort periode beheer en stabiliteit afgeleides van 'n ASK-13 sweeftuig vas te stel. Die kort periode beheer en stabiliteit afgeleides is verkry deur parameter afskatting op data wat gedurend vlugte van die sweeftuig opgeneem is. Die algoritme wat gebruik is om die parameters af te skat is die MMLE3 voorstelling van 'n maksimale moontlikheid afskatter. Om vlug data te versamel sensore moes in die sweeftuig geinstalleer word. Die sensore meet beheer oppervlak hoeke, versnellings, hoeksnellhede en die dinamies en statiese lugdruk om te verseker dat daar genoeg data is vir die afskatting. Om die afgeskatte parameters akkuraad te kry moet die loods spesefieke manoeuvres vlieg om seker te maak dat al die moduse van die sweeftuig is gestimuleer. Die resultate wat gelewer is 'n stel kort periode beheer en stabiliteit afgeleides wat nie akkuraad is nie, maar wat weI goed genoeg is or ie bewegings van die sweeftuig te simuleer. 2010-07-19T06:21:02Z 2010-07-19T06:21:02Z 2004-03 Thesis http://hdl.handle.net/10019.1/3631 en University of Stellenbosch application/pdf Stellenbosch : University of Stellenbosch
spellingShingle Control surface deflections
MMLE3 implementation
Dissertations -- Electronic engineering
Theses -- Electronic engineering
Gliders (Aeronautics)
Airplanes -- Flight testing
Flight control
Browne, Keith R.J.
The instrumentation and initial analysis of the short-term control and stability derivatives of an ASK-I3 glider
title The instrumentation and initial analysis of the short-term control and stability derivatives of an ASK-I3 glider
title_full The instrumentation and initial analysis of the short-term control and stability derivatives of an ASK-I3 glider
title_fullStr The instrumentation and initial analysis of the short-term control and stability derivatives of an ASK-I3 glider
title_full_unstemmed The instrumentation and initial analysis of the short-term control and stability derivatives of an ASK-I3 glider
title_short The instrumentation and initial analysis of the short-term control and stability derivatives of an ASK-I3 glider
title_sort instrumentation and initial analysis of the short term control and stability derivatives of an ask i3 glider
topic Control surface deflections
MMLE3 implementation
Dissertations -- Electronic engineering
Theses -- Electronic engineering
Gliders (Aeronautics)
Airplanes -- Flight testing
Flight control
url http://hdl.handle.net/10019.1/3631
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