Please use this identifier to cite or link to this item: https://www.um.edu.mt/library/oar/handle/123456789/95804
Title: Aircraft autoland system using fuzzy logic
Authors: Scerri, Matthew (2010)
Keywords: Fuzzy systems
Nautical instruments
Artificial intelligence
Issue Date: 2010
Citation: Scerri, M. (2010). Aircraft autoland system using fuzzy logic (Bachelor's dissertation).
Abstract: A full aircraft Autoland system using fuzzy logic has been developed. It is based on the flight model of a medium sized commercial airliner (Boeing 73 7-800), and was designed for a full 6 degree of freedom flight simulator. This was achieved by implementing several independent single output Fuzzy Controllers that are able to work together based on instrument readings continuously taken from the aircraft. Scenarios the solution was tested in include varying glidepath angles, various weather situations that include severe stable crosswinds and severe gusting crosswinds. For each case, the final results show that not only were safe landings performed in cases where the conditions were within the limitations set by the aircraft's manufacturer but also in worse conditions. These include landing in airports with a steep glidepath angle (such as London City Airport) but also landing in extreme crosswind conditions nearly double that of what the manufacturers recommend is used as a limitation.
Description: B.Sc. IT (Hons)(Melit.)
URI: https://www.um.edu.mt/library/oar/handle/123456789/95804
Appears in Collections:Dissertations - FacICT - 2010
Dissertations - FacICTAI - 2002-2014

Files in This Item:
File Description SizeFormat 
BSC(HONS)IT_Scerri_Matthew_2010.pdf
  Restricted Access
10.3 MBAdobe PDFView/Open Request a copy


Items in OAR@UM are protected by copyright, with all rights reserved, unless otherwise indicated.