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

AGUILAR CASTILLO, WILBERT GEOVANNY; PAREDES CALDERON, DARWIN MANOLO

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