prikaz prve stranice dokumenta Utjecaj dinamičkog kočenja propulzora na ponašanje mutlirotorske letjelice
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master's thesis
Utjecaj dinamičkog kočenja propulzora na ponašanje mutlirotorske letjelice
Zagreb: University of Zagreb, Faculty of Electrical Engineering and Computing, 2017. urn:nbn:hr:168:632362
Badanjek, Stribor
University of Zagreb
Faculty of Electrical Engineering and Computing

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Badanjek, S. (2017). Utjecaj dinamičkog kočenja propulzora na ponašanje mutlirotorske letjelice (Master's thesis). Zagreb: University of Zagreb, Faculty of Electrical Engineering and Computing. Retrieved from https://urn.nsk.hr/urn:nbn:hr:168:632362

Badanjek, Stribor. "Utjecaj dinamičkog kočenja propulzora na ponašanje mutlirotorske letjelice." Master's thesis, University of Zagreb, Faculty of Electrical Engineering and Computing, 2017. https://urn.nsk.hr/urn:nbn:hr:168:632362

Badanjek, Stribor. "Utjecaj dinamičkog kočenja propulzora na ponašanje mutlirotorske letjelice." Master's thesis, University of Zagreb, Faculty of Electrical Engineering and Computing, 2017. https://urn.nsk.hr/urn:nbn:hr:168:632362

Badanjek, S. (2017). 'Utjecaj dinamičkog kočenja propulzora na ponašanje mutlirotorske letjelice', Master's thesis, University of Zagreb, Faculty of Electrical Engineering and Computing, accessed 25 November 2024, https://urn.nsk.hr/urn:nbn:hr:168:632362

Badanjek S. Utjecaj dinamičkog kočenja propulzora na ponašanje mutlirotorske letjelice [Master's thesis]. Zagreb: University of Zagreb, Faculty of Electrical Engineering and Computing; 2017 [cited 2024 November 25] Available at: https://urn.nsk.hr/urn:nbn:hr:168:632362

S. Badanjek, "Utjecaj dinamičkog kočenja propulzora na ponašanje mutlirotorske letjelice", Master's thesis, University of Zagreb, Faculty of Electrical Engineering and Computing, Zagreb, 2017. Available at: https://urn.nsk.hr/urn:nbn:hr:168:632362

Metadata
TitleUtjecaj dinamičkog kočenja propulzora na ponašanje mutlirotorske letjelice
Title (english)Influence of Dynamic Braking of Propulsor on Multirotor UAV Performance
AuthorStribor Badanjek
MentorStjepan Bogdan (mentor)
Committee memberStjepan Bogdan (predsjednik povjerenstva)
Committee memberZdenko Kovačić (član povjerenstva)
Committee memberMatko Orsag (član povjerenstva)
GranterUniversity of Zagreb
Faculty of Electrical Engineering and Computing
Zagreb
Defense date and country2017-09-11, Croatia
Scientific / art field,
discipline and subdiscipline		TECHNICAL SCIENCES
Electrical Engineering
Abstract
Potreba za sve ve´com brzinom i agilnosti postavila je nove zahtjeve na dinamiku propulzora. U prvim se generacijama za koˇcenje propulzora koristio otpor zraka, dok novije generacije koriste dinamiˇcko koˇcenje propulzora. U ovom se radu ispituje utjecaj dinamicˇkog kocˇenja na ponašanje letjelice. U tu svrhu izrad¯en je simulink model letjelice kako bi se u kontroliranom i sigurnom okruženju mogli obaviti testovi. Napravljen je i niz stvarnih mjerenja na letjelici u svrhu validacije dobivenog modela. Za modeliranje propulzora korišteni su podatci o generiranom zakretnom momentu dobiveni pomoc´u izrad¯ene mjerne platforme. Tokom procesa validacije ustanovljeno je da ovako dobiveni model ne opisuje željenu dinamiku propulzora dovoljno dobro te ga nije mogu´ce koristiti u daljnjem razmatranju. Izvršena je površna analiza korištenjem mjerenja iz crne kutije. Uz ukljuˇceno dinami ˇcko koˇcenje dobivamo konzistentnije rezultate za razliˇcite vrijednosti gasa i širi raspon upravljaˇckih veliˇcina. Pri nižim obrtajima motora bez dinamiˇckog koˇcenja dolazi do oscilatornog vladanja, dok je vladanje u podruˇcju viših obrtaja prihvatljivije jer je otpor zraka ve´ci pa je i koˇcenje jaˇce.
Abstract (english)
The need for higher speed and agility has put new demands on propulsor dynamic. The first generations of propulsors used air resistance for braking while new generations use dynamic braking of propulsors. This paper tests the influence of dynamic braking on drone performance. A simulink drone model was made in order to run tests in a controlled and safe environment. A number of real measurements were taken on a drone in order to validate the obtained model. The data on generated torque used to model propulsors were obtained through the measuring platform were. During the validation it was established that the obtained model does not describe the desired dynamics of the propulsors well enough and it should not be used for further consideration. A cursory analysis was done using measurements from the black box. If we include dynamic braking, we get more consistent results for various throttle values and a wider range of control values. Oscilations occur at lower motor speed without dynamic braking while at higher speed the performance is more acceptable due to higher air resistance which enables better braking.
Keywords
Keywords (english)
Languagecroatian
URN:NBNurn:nbn:hr:168:632362
Study programmeTitle: Electrical Engineering and Information Technology
Study programme type: university
Study level: graduate
Academic / professional title: magistar/magistra inženjer/inženjerka elektrotehnike i informacijske tehnologije (magistar/magistra inženjer/inženjerka elektrotehnike i informacijske tehnologije)
Type of resourceText
File originBorn digital
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Created on2019-03-13 18:44:21