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Stall prevention control of fixed-wing unmanned aerial vehicles

Thesis (MScEng (Electrical and Electronic Engineering))--University of Stellenbosch, 2010.

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Bibliographic Details
Main Author: Basson, Matthys Michaelse
Other Authors: Peddle, I. K.
Format: Thesis
Language:English
Published: Stellenbosch : University of Stellenbosch 2010
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access_status_str Open Access
author Basson, Matthys Michaelse
author2 Peddle, I. K.
author_browse Basson, Matthys Michaelse
Peddle, I. K.
author_facet Peddle, I. K.
Basson, Matthys Michaelse
author_sort Basson, Matthys Michaelse
collection Thesis
dc_rights_str_mv University of Stellenbosch
description Thesis (MScEng (Electrical and Electronic Engineering))--University of Stellenbosch, 2010.
format Thesis
id oai:scholar.sun.ac.za:10019.1/4310
institution Stellenbosch University (South Africa)
language English
last_indexed 2026-06-10T12:43:33.723Z
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:10019.1/4310 Stall prevention control of fixed-wing unmanned aerial vehicles Basson, Matthys Michaelse Peddle, I. K. University of Stellenbosch. Faculty of Engineering. Dept. of Electrical and Electronic Engineering. Stall prevention Stall control Stall detection UAV Dissertations -- Electronic engineering Theses -- Electronic engineering Drone aircraft Stalling (Aerodynamics) Drone aircraft -- Stalling Thesis (MScEng (Electrical and Electronic Engineering))--University of Stellenbosch, 2010. ENGLISH ABSTRACT: This thesis presents the development of a stall prevention flight control subsystem, which can easily be integrated into existing flight control architectures of fixed-wing unmanned aerial vehicles (UAV’s). This research forms an important part of faulttolerant flight control systems and will ensure that the aircraft continues to operate safely within its linear aerodynamic region. The focus of this thesis was the stall detection and prevention problem. After a thorough literature study on the topic of stall, a model based stall prevention control algorithm with feedback from an angle of attack sensor was developed. This algorithm takes into account the slew rate and saturation limits of the aircraft’s servos and is able to predict when the current flight condition will result in stall. The primary concern was stall during wings-level flight and involved the prevention of stall by utilising only the elevator control surface. A model predictive slew rate control algorithm was developed to override and dynamically limit the elevator command to ensure that the angle of attack does not exceed a predefined limit. The stall prevention control system was designed to operate as a switching control scheme, to minimise any restrictions imposed on the existing flight control system. Finally, software in the loop simulations were conducted using a nonlinear aircraft model and realistic sensor noise, to verify the theoretical results obtained during the development of this stall prevention control strategy. A worst-case performance analysis was also conducted to investigate the robustness of the control algorithms against model uncertainties. AFRIKAANSE OPSOMMING: Hierdie tesis handel oor die ontwikkeling van ’n staak voorkomings-vlugbeheer substelsel wat maklik geïntegreer kan word in bestaande vlugbeheer argitektuur van onbemande vaste-vlerk lugvaartuie. Hierdie tesis vorm ’n belangrike deel van fouttolerante vlugbeheertegnieke en sal verseker dat die vliegtuig slegs binne sy lineêre aerodinamiese werksgebied bly. Die fokus van hierdie tesis is die staak opsporing en voorkomings probleem. Na afloop van ’n deeglike literatuurstudie oor die onderwerp van staak, is ’n model gebaseerde staak voorkomings-beheertegniek ontwikkel, wat terugvoer van ’n invalshoek sensor ontvang. Hierdie algoritme neem die sleur tempo en defleksie limiete van die vliegtuig se servos in ag en is in staat om staak te voorspel. Die primêre oorweging was staak tydens simmetriese vlugte en behels slegs die voorkoming van staak deur gebruik te maak van die hei beheer oppervlak. ’n Model voorspellings sleur tempo beheeralgoritme is ontwikkel om die hei-roer dinamies te beperk sodat die invalshoek nie ’n sekere vooraf bepaalde limiet oorskry nie. Die staak voorkomings beheerstelsel is ontwerp om te funksioneer as ’n skakel beheer skema om die beperkings op die bestaande vlugbeheerstelsel te minimaliseer. Laastens was sagteware-in-die-lus simulasies gebruik om die teoretiese resultate, wat verkry is tydens die ontwikkeling van hierdie staak voorkomings beheer-strategie, te kontroleer. Om die robuusthied van hierdie beheeralgoritmes teen model onsekerhede te ondersoek, is ’n ergste-geval prestasie analise ook uitgevoer. 2010-02-17T07:01:22Z 2010-08-13T15:01:30Z 2010-02-17T07:01:22Z 2010-08-13T15:01:30Z 2010-03 Thesis http://hdl.handle.net/10019.1/4310 en University of Stellenbosch 145 p. : ill. application/pdf Stellenbosch : University of Stellenbosch
spellingShingle Stall prevention
Stall control
Stall detection
UAV
Dissertations -- Electronic engineering
Theses -- Electronic engineering
Drone aircraft
Stalling (Aerodynamics)
Drone aircraft -- Stalling
Basson, Matthys Michaelse
Stall prevention control of fixed-wing unmanned aerial vehicles
title Stall prevention control of fixed-wing unmanned aerial vehicles
title_full Stall prevention control of fixed-wing unmanned aerial vehicles
title_fullStr Stall prevention control of fixed-wing unmanned aerial vehicles
title_full_unstemmed Stall prevention control of fixed-wing unmanned aerial vehicles
title_short Stall prevention control of fixed-wing unmanned aerial vehicles
title_sort stall prevention control of fixed wing unmanned aerial vehicles
topic Stall prevention
Stall control
Stall detection
UAV
Dissertations -- Electronic engineering
Theses -- Electronic engineering
Drone aircraft
Stalling (Aerodynamics)
Drone aircraft -- Stalling
url http://hdl.handle.net/10019.1/4310
work_keys_str_mv AT bassonmatthysmichaelse stallpreventioncontroloffixedwingunmannedaerialvehicles