Zobrazeno 1 - 10
of 15
pro vyhledávání: '"J. V. Caetano"'
Publikováno v:
2019 International Conference on Unmanned Aircraft Systems (ICUAS).
The current paper’s objective is to present the methodology used in the design of a class I unmanned aircraft (UA), intended for maritime surveillance, atmospheric pollution monitoring and search and rescue (SAR) missions. Its development encompass
Publikováno v:
International Journal of Micro Air Vehicles, 11
Despite significant interest in tailless flapping-wing micro aerial vehicle designs, tailed configurations are often favoured, as they offer many benefits, such as static stability and a simpler control strategy, separating wing and tail control. How
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::aff783606304d431944def396f59924c
http://hdl.handle.net/10044/1/69040
http://hdl.handle.net/10044/1/69040
Publikováno v:
2017 International Conference on Unmanned Aircraft Systems, ICUAS 2017
Although flapping-wing micro aerial vehicles have become a hot topic in academia, the knowledge we have of these systems, their force generation mechanisms and dynamics is still limited. Recent technological advances have allowed for the development
Publikováno v:
AIAA Modeling and Simulation Technologies Conference: 5-9 June 2017, Denver, Colorado
AIAA Modeling and Simulation Technologies Conference
AIAA Modeling and Simulation Technologies Conference
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::5d46eeb63a5e1f4bb01222811acb9031
http://resolver.tudelft.nl/uuid:a72dfb45-3ebf-4c0d-8d7e-ff449a1cab8b
http://resolver.tudelft.nl/uuid:a72dfb45-3ebf-4c0d-8d7e-ff449a1cab8b
Autor:
J. V. Caetano, G.C.H.E. de Croon, Bart Remes, C.C. de Visser, J.L. Verboom, C. De Wagter, Max Mulder
Publikováno v:
International Journal of Micro Air Vehicles. 5:273-286
This paper presents an approach to the system identification of the Delfly II Flapping Wing Micro Air Vehicle (FWMAV) using flight test data. It aims at providing simple FWMAV aerodynamic models that can be used in simulations as well as in nonlinear
Flapping-wing aerodynamic models that are accurate, computationally efficient and physically meaningful, are challenging to obtain. Such models are essential to design flapping-wing micro air vehicles and to develop advanced controllers enhancing the
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::53784e4420f51afee94ab41b601a9ebb
http://hdl.handle.net/10044/1/58782
http://hdl.handle.net/10044/1/58782
Publikováno v:
IROS
Publikováno v:
Handbook of Unmanned Aerial Vehicles ISBN: 9789048197064
Handbook of Unmanned Aerial Vehicles
Handbook of Unmanned Aerial Vehicles
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::dee253ff952218bbb180add087f8be83
https://doi.org/10.1007/978-90-481-9707-1_80
https://doi.org/10.1007/978-90-481-9707-1_80
Autor:
J. V. Caetano, G.C.H.E. de Croon, C. De Wagter, C.C. de Visser, Bart Remes, B. W. van Oudheusden, Max Mulder, Mustafa Percin
Publikováno v:
2014 International Conference on Unmanned Aircraft Systems (ICUAS).
The determination of dynamic forces acting on a Flapping Wing Micro Aerial Vehicle (FWMAV) is a challenging task due to the unsteady nature of force generation mechanisms. To assure a proper force identification in future researches, this work compar
Autor:
J. V. Caetano, G.C.H.E. de Croon, Max Mulder, M. B. Weehuizen, Bart Remes, C.C. de Visser, C. De Wagter
Publikováno v:
2014 International Conference on Unmanned Aircraft Systems (ICUAS).
Several studies have focused on deriving kinematic formulations of simulated flapping wing micro air vehicles (FWMAV). However, very few used real-life flight data and none have compared the predicted aerodynamic forces and moments across different k