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A comparison of control systems for the flight transition of VTOL unmanned aerial vehicles

Thesis (MScEng (Electrical and Electronic Engineering))--University of Stellenbosch, 2009.

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Bibliographic Details
Main Author: Kriel, Steven Cornelius
Other Authors: Jones, T.
Format: Thesis
Language:English
Published: Stellenbosch : University of Stellenbosch 2008
Subjects:
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access_status_str Open Access
author Kriel, Steven Cornelius
author2 Jones, T.
author_browse Jones, T.
Kriel, Steven Cornelius
author_facet Jones, T.
Kriel, Steven Cornelius
author_sort Kriel, Steven Cornelius
collection Thesis
dc_rights_str_mv University of Stellenbosch
description Thesis (MScEng (Electrical and Electronic Engineering))--University of Stellenbosch, 2009.
format Thesis
id oai:scholar.sun.ac.za:10019.1/1535
institution Stellenbosch University (South Africa)
language English
last_indexed 2026-06-10T12:46:40.081Z
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:10019.1/1535 A comparison of control systems for the flight transition of VTOL unmanned aerial vehicles Kriel, Steven Cornelius Jones, T. University of Stellenbosch. Faculty of Engineering. Dept. of Electrical and Electronic Engineering. Theses -- Electrical and electronic engineering Dissertations -- Electrical and electronic engineering Drone aircraft Linear control systems Flight control Thesis (MScEng (Electrical and Electronic Engineering))--University of Stellenbosch, 2009. This thesis details the development of linear control systems that allow a vertical take-off and landing unmanned aerial vehicle to perform transitions between vertical and horizontal flight. Two mathematical models are derived for the control system design. A large non-linear model, describing all the dynamics of the aircraft, is linearised in order to perform optimal control using linear quadratic regulator theory. Another model is decoupled using time scale separation to form separate rigid body and point mass dynamics. The decoupled model is controlled using classical control techniques. Simulation results are used to judge the relative performance of the two control schemes in several fields including: Trajectory tracking, sensitivity to parameters, computational complexity and ease of use. 2008-08-12T09:00:31Z 2010-06-01T08:26:52Z 2008-08-12T09:00:31Z 2010-06-01T08:26:52Z 2008-03 Thesis http://hdl.handle.net/10019.1/1535 en University of Stellenbosch application/pdf Stellenbosch : University of Stellenbosch
spellingShingle Theses -- Electrical and electronic engineering
Dissertations -- Electrical and electronic engineering
Drone aircraft
Linear control systems
Flight control
Kriel, Steven Cornelius
A comparison of control systems for the flight transition of VTOL unmanned aerial vehicles
title A comparison of control systems for the flight transition of VTOL unmanned aerial vehicles
title_full A comparison of control systems for the flight transition of VTOL unmanned aerial vehicles
title_fullStr A comparison of control systems for the flight transition of VTOL unmanned aerial vehicles
title_full_unstemmed A comparison of control systems for the flight transition of VTOL unmanned aerial vehicles
title_short A comparison of control systems for the flight transition of VTOL unmanned aerial vehicles
title_sort comparison of control systems for the flight transition of vtol unmanned aerial vehicles
topic Theses -- Electrical and electronic engineering
Dissertations -- Electrical and electronic engineering
Drone aircraft
Linear control systems
Flight control
url http://hdl.handle.net/10019.1/1535
work_keys_str_mv AT krielstevencornelius acomparisonofcontrolsystemsfortheflighttransitionofvtolunmannedaerialvehicles
AT krielstevencornelius comparisonofcontrolsystemsfortheflighttransitionofvtolunmannedaerialvehicles