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Brezžični vmesnik za Pitotovo cev : diplomsko delo
Kren, Matevž (Author), Bulić, Patricio (Mentor) More about this mentor... This link opens in a new window

URLURL - Presentation file, Visit http://eprints.fri.uni-lj.si/2801/ This link opens in a new window

Abstract
Pitotova cev je priprava za merjenje pritiska, s katero lahko določimo hitrosti tekočin z znano gostoto. Največkrat se uporablja za izračun hitrosti zračnih in vodnih plovil. Pitotove cevi novih modelov letal, ki so spremenjene oblike in jih želimo certificirati, je potrebno umeriti in s tem pokazati, da motnje zračnega pretoka v okolici letala ne vplivajo na natančnost meritev. Cilj diplomskega dela je bila priprava brezžičnega vmesnika, ki bi postopek poenostavil in pohitril. V ta namen je bil razvit vgrajeni sistem za zajem in beleženje podatkov iz senzorjev Pitotove cevi in njihovo prikazovanje v pilotski kabini. Osrednji del brezžičnega vmesnika predstavljata razvojni plošči STM32F4-Discovery, ki prenos podatkov nadzirata z upravljanjem brezžičnih modulov ALPHA-TRX433S.

Language:Slovenian
Keywords:Pitotova cev, vgrajeni sistem, STM32F4-Discovery, brezžični vmesnik, računalništvo, visokošolski strokovni študij, računalništvo in informatika, diplomske naloge
Work type:Bachelor thesis/paper (mb11)
Tipology:2.11 - Undergraduate Thesis
Organization:FRI - Faculty of computer and information science
Year:2014
Publisher:[M. Kren]
Number of pages:38 str.
UDC:004.5:629.7(043.2)
COBISS.SI-ID:1536034243 Link is opened in a new window
Views:840
Downloads:160
Metadata:XML RDF-CHPDL DC-XML DC-RDF
 
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Secondary language

Language:English
Title:A wireless interface for the Pitote tube
Abstract:
A pitot tube is a pressure measurement instrument used to measure fluid flow velocity. Most often, pitot tubes are used to determine the speed of aircraft and boats. Before launching a new aircraft design for use in both private and commercial aviation, it must be shown the correct airspeed data is communicated regardless of airflow disruptions. This is achieved through calibration of the pitot tubes. In this dissertation, we focus on developing a wireless interface to achieve a faster and improved data transmission without fuselage alteration. For this purpose, an embedded system was designed. It integrates the STM32F4-Discovery development environment and the ALPHA-TRX433S high performance radio modules. In essence, data is collected and wirelessly transmitted for display.

Keywords:Pitot tube, embedded system, STM32F4-Discovery, wireless interface, computer science, computer and information science, diploma

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