FuzzyTail

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dc.contributor.author	Kostelidis, Iordanis
dc.date.accessioned	2025-06-11T10:17:26Z
dc.date.issued	2025-06-16
dc.description.abstract	FuzzyTail is a control system for an aircraft’s vertical flight angle using the rear control surface angle, based on fuzzy logic and implemented in MATLAB/Simulink.
dc.identifier.uri	https://repository.kostelidis.dev/handle/123456789/44
dc.language.iso	el
dc.title	FuzzyTail
dc.type	Term Paper

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Name:: FuzzyTail.pdf
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Name:: FuzzyTail - Presentation.pdf
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Name:: FuzzyTail - Presentation.pptx
Size:: 1.99 MB
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Format:: Microsoft Word XML

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