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Title:MIKROKRMILNIŠKO NADZIRAN INDIKATOR VAROVALK
Authors:ID Hrastnik, Boris (Author)
ID Vlaovič, Boštjan (Mentor) More about this mentor... New window
ID Zunanji, Sodelavec (Comentor)
Files:.pdf VS_Hrastnik_Boris_2015.pdf (3,64 MB)
MD5: FD0D8F2DC5730A4481B0D664B70DF23C
 
Language:Slovenian
Work type:Bachelor thesis/paper
Typology:2.11 - Undergraduate Thesis
Organization:FERI - Faculty of Electrical Engineering and Computer Science
Abstract:Diplomsko delo opisuje izdelavo indikatorja varovalk za jadralno letalo. Indikator varovalk je del sistema za nadzor napajanja jadralnega letala. Pri zasnovi inštrumenta je velikost določala prostor v čelni plošči jadralnega letala. Indikator mora imeti tudi hiter in zanesljiv odziv, zato smo uporabili komunikacijo CAN. Uvodno predstavimo problem in funkcionalne zahteve inštrumenta. V nadaljevanju opišemo izbrano strojno opremo in postopek izdelave prototipa, vključno s programsko opremo. V zaključku podamo rezultate testov, ki so potrdili skladnost s podanimi zahtevami.
Keywords:Indikator, mikroprocesor, CAN komunikacija, jadralno letalo
Place of publishing:Maribor
Publisher:[B. Hrastnik]
Year of publishing:2015
PID:20.500.12556/DKUM-54806 New window
UDC:621.38.049.77(043.2)
COBISS.SI-ID:19250198 New window
NUK URN:URN:SI:UM:DK:ZQNZZFJV
Publication date in DKUM:30.10.2015
Views:2447
Downloads:146
Metadata:XML DC-XML DC-RDF
Categories:KTFMB - FERI
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Secondary language

Language:English
Title:MICROCONTROLLER BASED FUSE INDICATOR
Abstract:The thesis describes the production of fuse indicator for glider. The fuse indicator is a part of the glider power control system. In the design of the instrument the size provided the space in the front panel of the glider. The indicator has to have a fast and reliable response, that is why we used the communication CAN. In the introduction we present the problem and the functional requirements of the instrument. We continue with the description of the chosen hardware and the process of the production of a prototype, including the software. In the conclusion we present the results of the tests that have confirmed the compatibility with the given requirements.
Keywords:indicator, microprocessor, CAN communication, glider


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