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MATH MODEL OF UAV MULTI ROTOR PROTOTYPE WITH FIXED WING AERODYNAMIC STRUCTURE FOR A FLIGHT SIMULATOR

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dc.contributor.author AGUILAR CASTILLO, WILBERT GEOVANNY
dc.contributor.author PAREDES CALDERON, DARWIN MANOLO
dc.date.accessioned 2019-05-14T00:37:32Z
dc.date.available 2019-05-14T00:37:32Z
dc.date.issued 2017-06-08
dc.identifier.idautor 0703844696
dc.identifier.idautor 1803138005
dc.identifier.issn 0302-9743
dc.identifier.uri https://doi.org/10.1007/978-3-319-60922-5_15
dc.identifier.uri https://link.springer.com/chapter/10.1007/978-3-319-60922-5_15
dc.identifier.uri http://repositorio.espe.edu.ec/handle/21000/19914
dc.publisher LECTURE NOTES IN COMPUTER SCIENCE
dc.relation.ispartof LECTURE NOTES IN COMPUTER SCIENCE, volumen 10325
dc.rights openAccess
dc.title MATH MODEL OF UAV MULTI ROTOR PROTOTYPE WITH FIXED WING AERODYNAMIC STRUCTURE FOR A FLIGHT SIMULATOR
dc.type Artículo


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