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Includes abstract.
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| Other Authors: | |
| Format: | Thesis |
| Language: | English |
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Department of Chemical Engineering
2014
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| _version_ | 1867613194562830336 |
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| access_status_str | Open Access |
| author | Johnson, Bruce Edward |
| author2 | Verrinder, Robyn |
| author_browse | Johnson, Bruce Edward Verrinder, Robyn |
| author_facet | Verrinder, Robyn Johnson, Bruce Edward |
| author_sort | Johnson, Bruce Edward |
| collection | Thesis |
| description | Includes abstract. |
| format | Thesis |
| id | oai:open.uct.ac.za:11427/5310 |
| institution | University of Cape Town (South Africa) |
| language | eng |
| last_indexed | 2026-06-10T12:32:13.078Z |
| license_str | Not specified — see source repository |
| provenance_str_mv | Harvested via OAI-PMH from UCTD — University of Cape Town Open Access Repository |
| publishDate | 2014 |
| publishDateRange | 2014 |
| publishDateSort | 2014 |
| publisher | Department of Chemical Engineering |
| publisherStr | Department of Chemical Engineering |
| record_format | dspace |
| source_str | UCTD — University of Cape Town Open Access Repository |
| spelling | oai:open.uct.ac.za:11427/5310 An aircraft and provide information about flight performance and local microclimate Johnson, Bruce Edward Verrinder, Robyn Ginsberg, Samuel Engineering Includes abstract. Includes bibliographical references The application of using Unmanned Aerial Vehicles (UAVs) to locate thermal updraft currentsis a relatively new topic. It was first proposed in 1998 by John Wharington, and, subsequently, several researchers have developed algorithms to search and exploit thermals. However, few people have physically implemented a system and performed field testing. The aim of this project was to develop a low cost system to be carried on a glider to detect thermals effectively. A system was developed from the ground up and consisted of custom hardware and software that was developed specifically for aircraft. Data fusion was performed to estimate the attitude of the aircraft; this was done using a direction cosine (DCM) based method. Altitude and airspeed data were fused by estimating potential and kinetic energy respectively; thus determining the aircraft’s total energy. This data was then interpreted to locate thermal activity. The system comprised an Inertial Measurement Unit (IMU), airspeed sensor, barometric altitude sensor, Global Positioning System (GPS), temperature sensor, SD card and a realtime telemetry link. These features allowed the system to determine aircraft position, height, airspeed and air temperature in realtime. A custom-designed radio controlled (RC) glider was constructed from composite materials in addition to a second 3.6 m production glider that was used during flight testing. Sensor calibration was done using a wind tunnel with custom designed apparatus that allowed a complete wing with its pitot tube to be tested in one operation. Flight testing was conducted in the field at several different locations over the course of six months. A total of 25 recorded flights were made during this period. Both thermal soaring and ridge soaring were performed to test the system under varying weather conditions. A telemetry link was developed to transfer data in realtime from the aircraft to a custom ground station. The recorded results were post-processed using Matlab and showed that the system was able to detect thermal updrafts. The sensors used in the system were shown to provide acceptable performance once some calibration had been performed. Sensor noise proved to be problematic, and time was spent alleviating its effects. 2014-07-31T11:09:11Z 2014-07-31T11:09:11Z 2013 Master Thesis Masters MSc http://hdl.handle.net/11427/5310 eng application/pdf Department of Chemical Engineering Faculty of Engineering and the Built Environment University of Cape Town |
| spellingShingle | Engineering Johnson, Bruce Edward An aircraft and provide information about flight performance and local microclimate |
| thesis_degree_str | Master's |
| title | An aircraft and provide information about flight performance and local microclimate |
| title_full | An aircraft and provide information about flight performance and local microclimate |
| title_fullStr | An aircraft and provide information about flight performance and local microclimate |
| title_full_unstemmed | An aircraft and provide information about flight performance and local microclimate |
| title_short | An aircraft and provide information about flight performance and local microclimate |
| title_sort | aircraft and provide information about flight performance and local microclimate |
| topic | Engineering |
| url | http://hdl.handle.net/11427/5310 |
| work_keys_str_mv | AT johnsonbruceedward anaircraftandprovideinformationaboutflightperformanceandlocalmicroclimate AT johnsonbruceedward aircraftandprovideinformationaboutflightperformanceandlocalmicroclimate |