Modeling of the Electronic Variable Pitch Drive

Kód výsledku v IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F61989100%3A27230%2F15%3A86094112" target="_blank" >RIV/61989100:27230/15:86094112 - isvavai.cz</a>

Výsledek na webu

<a href="http://dx.doi.org/10.1109/CarpathianCC.2015.7145062" target="_blank" >http://dx.doi.org/10.1109/CarpathianCC.2015.7145062</a>

DOI - Digital Object Identifier

<a href="http://dx.doi.org/10.1109/CarpathianCC.2015.7145062" target="_blank" >10.1109/CarpathianCC.2015.7145062</a>

Jazyk výsledku

angličtina

Název v původním jazyce

Modeling of the Electronic Variable Pitch Drive

Popis výsledku v původním jazyce

This contribution describes procedures and results obtained at the Department of Control Systems and Instrumentation of the VrB-Technical University of Ostrava during research and mathematical modelling of variable pitch systems behavior. The wiring scheme and control strategy of the electronic variable pitch drive mounted on new testing stand are presented. Ability of machines to fly had been based on the complex mechanical units until the end of last century. Development of high-quality and affordablesensors brings the innovation to this sector. The presented stand was created for testing of the new optimized control algorithms for UAV devices (multicopter). The complex mechanical parts can be replaced by electronics. The construction of EVP testingstand includes BLDC motor, power electronics (ESC), microcontroller, sensors and simple frame. It doesn't require complex mechanical parts. Management and control is compared with conventional helicopter eased considerably

Název v anglickém jazyce

Modeling of the Electronic Variable Pitch Drive

Popis výsledku anglicky

This contribution describes procedures and results obtained at the Department of Control Systems and Instrumentation of the VrB-Technical University of Ostrava during research and mathematical modelling of variable pitch systems behavior. The wiring scheme and control strategy of the electronic variable pitch drive mounted on new testing stand are presented. Ability of machines to fly had been based on the complex mechanical units until the end of last century. Development of high-quality and affordablesensors brings the innovation to this sector. The presented stand was created for testing of the new optimized control algorithms for UAV devices (multicopter). The complex mechanical parts can be replaced by electronics. The construction of EVP testingstand includes BLDC motor, power electronics (ESC), microcontroller, sensors and simple frame. It doesn't require complex mechanical parts. Management and control is compared with conventional helicopter eased considerably

Druh

D - Stať ve sborníku

CEP obor

JB - Senzory, čidla, měření a regulace

OECD FORD obor

—

Projekt

—

Návaznosti

S - Specificky vyzkum na vysokych skolach

Rok uplatnění

2015

Kód důvěrnosti údajů

S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Název statě ve sborníku

Proceedings of the 2015 16th International Carpathian Control Conference, ICCC 2015

ISBN

978-1-4799-7370-5

ISSN

—

e-ISSN

—

Počet stran výsledku

4

Strana od-do

138 - 141

Název nakladatele

Institute of Electrical and Electronics Engineers

Místo vydání

New York

Místo konání akce

Szilvasvarad

Datum konání akce

27. 5. 2015

Typ akce podle státní příslušnosti

WRD - Celosvětová akce

Kód UT WoS článku

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