Please use this identifier to cite or link to this item: https://repository.sustech.edu/handle/123456789/4690
Full metadata record
DC FieldValueLanguage
dc.contributor.authorAhmed, Elnail Kamal Eldin Idris
dc.contributor.authorSupervisor ,- Awadalla Taifour Ali
dc.date.accessioned2014-04-28T09:23:13Z
dc.date.available2014-04-28T09:23:13Z
dc.date.issued2012-01-01
dc.identifier.citationAhmed,Elnail Kamal Eldin Idris .DESIGN OF AIRCRAFT LANDING CONTROL SYSTEM USING FUZZY LOGIC/Elnail Kamal Eldin Idris Ahmed; Awadalla Taifour Ali.-Khartoum:Sudan University of Science and Technology,College of Engineering,2012.-90p. : ill. ; 28cm.-Ms.c.en_US
dc.identifier.urihttp://repository.sustech.edu/handle/123456789/4690
dc.descriptionThesisen_US
dc.description.abstractSince the Climate factors have strong negative effect on the process of landing, which makes crew needs a proper automatic landing system, to reduce the total landing cost by landing the aircraft at prescribed time. This project presents an intelligent control scheme that use a fuzzy logic controller in automatic aircraft landing control that will make the automatic landing systems (ALS) more intelligent. A design methodology has been proposed based on conventional control and repeated using fuzzy logic. The main goal of this research is to design a fuzzy logic controller to aid in landing the aircraft safely in all weather conditions. To examine the fuzzy controller performance, MATLAB fuzzy tool box is used.en_US
dc.description.sponsorshipSudan University of Science and Technologyen_US
dc.language.isoenen_US
dc.publisherSudan University of Science and Technologyen_US
dc.subjectElectrical Engineeringen_US
dc.subjectMicroprocessor and Controlen_US
dc.subjectAIRCRAFT LANDINGen_US
dc.subjectFUZZY LOGICen_US
dc.subjectAirophnesen_US
dc.titleDESIGN OF AIRCRAFT LANDING CONTROL SYSTEM USING FUZZY LOGICen_US
dc.title.alternative‫تصميم نظام تحكم في هبوط الطائرة بإستخدام‬ ‫المنطق الغامض‬en_US
dc.typeThesisen_US
Appears in Collections:Masters Dissertations : Engineering

Files in This Item:
File Description SizeFormat 
DESIGN OF AIRCRAFT LANDING ... .pdftitle831.46 kBAdobe PDFView/Open
Research .pdf
  Restricted Access
Research 2.03 MBAdobe PDFView/Open Request a copy


Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.