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Methods of parameter identification used in the field of helicopters

Thesis (MEng (Mechanics)) -- University of Stellenbosch, 1990.

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Bibliographic Details
Main Author: Fitzhenry, Geoffrey Alan
Other Authors: Pienaar, D. van V.
Format: Thesis
Language:English
Published: Stellenbosch : Stellenbosch University 2012
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access_status_str Open Access
author Fitzhenry, Geoffrey Alan
author2 Pienaar, D. van V.
author_browse Fitzhenry, Geoffrey Alan
Pienaar, D. van V.
author_facet Pienaar, D. van V.
Fitzhenry, Geoffrey Alan
author_sort Fitzhenry, Geoffrey Alan
collection Thesis
dc_rights_str_mv Stellenbosch University
description Thesis (MEng (Mechanics)) -- University of Stellenbosch, 1990.
format Thesis
id oai:scholar.sun.ac.za:10019.1/68871
institution Stellenbosch University (South Africa)
language English
last_indexed 2026-06-10T12:41:12.661Z
license_str Other — see source repository
provenance_str_mv Harvested via OAI-PMH from SUNScholar — Stellenbosch University Repository
publishDate 2012
publishDateRange 2012
publishDateSort 2012
publisher Stellenbosch : Stellenbosch University
publisherStr Stellenbosch : Stellenbosch University
record_format dspace
source_str SUNScholar — Stellenbosch University Repository
spelling oai:scholar.sun.ac.za:10019.1/68871 Methods of parameter identification used in the field of helicopters Fitzhenry, Geoffrey Alan Pienaar, D. van V. Stellenbosch University. Faculty of Engineering. Dept. of Mechanical and Mechatronic Engineering. System identification Helicopters -- Recognition Dissertations -- Mechanical engineering Thesis (MEng (Mechanics)) -- University of Stellenbosch, 1990. Three identification techniques most generally used in the field of helicopter flight mechanics are explained and discussed.The lesser used Instrumental Variable method is briefly explained and compared to the more popular methods but not applied to any data in the scope of this report.The Least Squares method is applied to a simulated two-input-two-output second order system with identified parameter errors in the order of 0.73 % for the case of small additive noise. The method, although popular, is generally used to obtain starting estimates for the more popular Maximum Likelihood method.The Maximum Likelihood method is applied to the model of a suspended solid cylindrical body in order to estimate the inertial properties of the body. Unfortunately due to inaccuracies in the calibration of the displacement and force sensors of the practical experiment, percentage differences between analytical and experimental results of up to 8.83 % were obtained. Although the results are not as close as was expected, the concept provides a compact method of identifying both the centre of gravity location and the inertial properties of a body. Masters 2012-08-27T12:26:48Z 2012-08-27T12:26:48Z 1990 Thesis http://hdl.handle.net/10019.1/68871 en Stellenbosch University 126 pages : ill. application/pdf Stellenbosch : Stellenbosch University
spellingShingle System identification
Helicopters -- Recognition
Dissertations -- Mechanical engineering
Fitzhenry, Geoffrey Alan
Methods of parameter identification used in the field of helicopters
title Methods of parameter identification used in the field of helicopters
title_full Methods of parameter identification used in the field of helicopters
title_fullStr Methods of parameter identification used in the field of helicopters
title_full_unstemmed Methods of parameter identification used in the field of helicopters
title_short Methods of parameter identification used in the field of helicopters
title_sort methods of parameter identification used in the field of helicopters
topic System identification
Helicopters -- Recognition
Dissertations -- Mechanical engineering
url http://hdl.handle.net/10019.1/68871
work_keys_str_mv AT fitzhenrygeoffreyalan methodsofparameteridentificationusedinthefieldofhelicopters