Full Text Available

Note: Clicking the button above will open the full text document at the original institutional repository in a new window.

Development of a Low-Cost, Low-Weight Flight Control System for an Electrically Powered Model Helicopter

Thesis (MScEng (Electrical and Electronic Engineering))--University of Stellenbosch, 2005.

Saved in:
Bibliographic Details
Main Author: Carstens, Nicol
Other Authors: Milne, G. W.
Format: Thesis
Language:English
Published: Stellenbosch : University of Stellenbosch 2008
Subjects:
Tags: Add Tag
No Tags, Be the first to tag this record!
_version_ 1867613912229216256
access_status_str Open Access
author Carstens, Nicol
author2 Milne, G. W.
author_browse Carstens, Nicol
Milne, G. W.
author_facet Milne, G. W.
Carstens, Nicol
author_sort Carstens, Nicol
collection Thesis
dc_rights_str_mv University of Stellenbosch
description Thesis (MScEng (Electrical and Electronic Engineering))--University of Stellenbosch, 2005.
format Thesis
id oai:scholar.sun.ac.za:10019.1/1640
institution Stellenbosch University (South Africa)
language English
last_indexed 2026-06-10T12:43:40.919Z
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:10019.1/1640 Development of a Low-Cost, Low-Weight Flight Control System for an Electrically Powered Model Helicopter Carstens, Nicol Milne, G. W. University of Stellenbosch. Faculty of Engineering. Dept. of Electrical and Electronic Engineering. Theses -- Electronic engineering Theses -- Computer science Dissertations -- Computer science Dissertations -- Electronic engineering Helicopters -- Control systems Drone aircraft Helicopters -- Models Thesis (MScEng (Electrical and Electronic Engineering))--University of Stellenbosch, 2005. This project started a new research area in rotary-wing °ight control in the Computer and Control group at the University of Stellenbosch. Initial attempts to build a quad-rotor vehicle exposed di±culties which motivated changing to a standard model helicopter as a test vehicle. A JR Voyager E electrically powered model helicopter was instrumented with low-cost, low-weight sensors and a data communication RF link. The total cost of the sensor, communication and microcontroller hardware used is approximately US$ 1000 and the added onboard hardware weighs less than 0:4 kg. The sensors used to control the helicopter include a non-di®erential u-Blox GPS receiver, Analog Devices ADXRS150 rate gyroscopes, Analog Devices ADXL202 accelerometers, a Polaroid ultrasonic range sensor and a Honeywell HMC2003 magnetometer. Successful yaw, height and longitudinal position control was demonstrated. Signi¯cant further work is proposed, based on the literature study performed and the insights and achievements of the ¯rst rotary-wing unmanned aerial vehicle project in the group. 2008-07-01T09:53:21Z 2010-06-01T08:29:19Z 2008-07-01T09:53:21Z 2010-06-01T08:29:19Z 2005-03 Thesis http://hdl.handle.net/10019.1/1640 en University of Stellenbosch application/pdf Stellenbosch : University of Stellenbosch
spellingShingle Theses -- Electronic engineering
Theses -- Computer science
Dissertations -- Computer science
Dissertations -- Electronic engineering
Helicopters -- Control systems
Drone aircraft
Helicopters -- Models
Carstens, Nicol
Development of a Low-Cost, Low-Weight Flight Control System for an Electrically Powered Model Helicopter
title Development of a Low-Cost, Low-Weight Flight Control System for an Electrically Powered Model Helicopter
title_full Development of a Low-Cost, Low-Weight Flight Control System for an Electrically Powered Model Helicopter
title_fullStr Development of a Low-Cost, Low-Weight Flight Control System for an Electrically Powered Model Helicopter
title_full_unstemmed Development of a Low-Cost, Low-Weight Flight Control System for an Electrically Powered Model Helicopter
title_short Development of a Low-Cost, Low-Weight Flight Control System for an Electrically Powered Model Helicopter
title_sort development of a low cost low weight flight control system for an electrically powered model helicopter
topic Theses -- Electronic engineering
Theses -- Computer science
Dissertations -- Computer science
Dissertations -- Electronic engineering
Helicopters -- Control systems
Drone aircraft
Helicopters -- Models
url http://hdl.handle.net/10019.1/1640
work_keys_str_mv AT carstensnicol developmentofalowcostlowweightflightcontrolsystemforanelectricallypoweredmodelhelicopter