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A model of small airship's propelling

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dc.title A model of small airship's propelling en
dc.contributor.author Adámek, Milan
dc.contributor.author Pospíšilík, Martin
dc.contributor.author Neumann, Petr
dc.contributor.author Silva, Rui Miguel Soares
dc.relation.ispartof Proceedings - 29th European Conference on Modelling and Simulation, ECMS 2015
dc.identifier.isbn 9780993244001
dc.date.issued 2015
dc.citation.spage 320
dc.citation.epage 326
dc.event.title 29th European Conference on Modelling and Simulation, ECMS 2015
dc.event.location Varna
utb.event.state-en Bulgaria
utb.event.state-cs Bulharsko
dc.event.sdate 2015-05-26
dc.event.edate 2015-05-29
dc.type conferenceObject
dc.language.iso en
dc.publisher European Council for Modelling and Simulation (ECMS)
dc.identifier.doi 10.7148/2015-0320
dc.relation.uri http://www.scs-europe.net/dlib/2015/2015-0320.htm
dc.relation.uri http://www.scs-europe.net/dlib/2015/ecms2015acceptedpapers/0320-mct_ECMS2015_0059.pdf
dc.subject Autonomous airship en
dc.subject Model en
dc.subject Propelling en
dc.subject Simulation of airship's motion en
dc.description.abstract For the purposes of development of a small and autonomously operated airship, a need to create a model of its propelling and motion has arisen. Being described within this paper, the model defines the requirements that are imposed to motors, propellers and the airship's controlling system. The model is based on a typical design of a small airship, that consists of two main propellers, being placed symetrically according to the gondola beneath the airship's bladder, and one tail propeller that is placed transversely at the airship's tail. According to this model, forces needed to move the airship in the desired direction can be estimated as well as the power consumption of the motors and angular velocity of the propellers. Although the dynamic model of the airship would exceed the framework of this paper, it is also described in broad terms and the results of two main simulations are presented hereby. The simulations describe the behavior of the airship in case of forward acceleration and braking as well as in case of yawing with such braking that ensures reaching of the desired yawing angle. © ECMS Valeri M. Mladenov, Petia Georgieva, Grisha Spasov, Galidiya Petrova (Editors). en
utb.faculty Faculty of Applied Informatics
dc.identifier.uri http://hdl.handle.net/10563/1005311
utb.identifier.obdid 43873958
utb.identifier.scopus 2-s2.0-84938697181
utb.source d-scopus
dc.date.accessioned 2015-09-09T15:16:38Z
dc.date.available 2015-09-09T15:16:38Z
utb.contributor.internalauthor Adámek, Milan
utb.contributor.internalauthor Pospíšilík, Martin
utb.contributor.internalauthor Neumann, Petr
utb.fulltext.affiliation Milan Adamek, Martin Pospisilik, Petr Neumann, Rui Miguel Soares Silva, Faculty of Applied Informatics Tomas Bata University in Zlin Nad Stranemi 4511, 76005 Zlin, Czech Republic E-mail: {adamek, pospisilik, neumann}@fai.utb.cz Lab UbiNET – Computer Science Security and Cybercrime Polytechnic Institute of Beja Rua Pedro Soares, 7800-295 Beja Portugal E-mail: ruisilva@acm.org
utb.fulltext.dates -
utb.fulltext.faculty Faculty of Applied Informatics
utb.fulltext.faculty Faculty of Applied Informatics
utb.fulltext.faculty Faculty of Applied Informatics
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