Zobrazeno 1 - 10
of 25
pro vyhledávání: '"Pandža, Viktor"'
Publikováno v:
In Acta Astronautica May 2022 194:83-92
Publikováno v:
In Aerospace Science and Technology November 2020 106
Publikováno v:
In Aerospace Science and Technology February 2020 97
Akademický článek
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Autor:
Pandža, Viktor
Insect flight capabilities provide fascination for humans and fuel aspirations for development and manufacturing of insect-type flapping wing aerial vehicles. However, complex underlying aerodynamic phenomena limit our abilities in understanding inse
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=od______9595::06a9be10f775575db5fb3193557ea928
https://repozitorij.fsb.unizg.hr/islandora/object/fsb:8053/datastream/PDF
https://repozitorij.fsb.unizg.hr/islandora/object/fsb:8053/datastream/PDF
NASA's Ingenuity Mars Helicopter has recently performed the first powered controlled flight on another planet. However, in spite of success of this mission, rotary wing solution might not be the optimal technology for flying in thin Martian atmospher
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=57a035e5b1ae::f8c95228a9408149cc9657c7ab13861d
https://www.bib.irb.hr/1173160
https://www.bib.irb.hr/1173160
Insect-like flapping-wing vehicle (FWV) concepts have great potential that implies excellent aerial capabilities, like hovering, robustness, great maneuverability, and very efficient flight in low Reynolds number regimes. However, complex multiphysic
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=57a035e5b1ae::eadc8d1879b9e212ae5808767b488c5f
https://www.bib.irb.hr/1145394
https://www.bib.irb.hr/1145394
Akademický článek
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In this work we study dynamics of flapping-wing micro unmanned aerial vehicle (MUAV) of the insect type. We present a novel control algorithm based on the reduced mechanical model and Discrete Mechanics and Optimal Control (DMOC) approach. In recent
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=57a035e5b1ae::ce3d4b0be0ed5962e033a51ff9930df9
https://www.bib.irb.hr/1146510
https://www.bib.irb.hr/1146510
In order to study dynamics of flapping wing moving at low Reynolds number in ambient fluid, we adopt geometric modelling approach of fully coupled wing-fluid system, incorporating Boundary Integral Method for calculating added masses, and Lie group r
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=57a035e5b1ae::2e1a26a1ffc17fc00f7a3e981ce4aa48
https://www.bib.irb.hr/947179
https://www.bib.irb.hr/947179