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Theoretical and practical investigation into the use of a bio-inspired “click” mechanism for the flight motor of a micro air vehicle
(2017-06-01)
Recently, flapping wing micro air vehicles have received great attention with the drive to make smaller and smaller devices. This paper describes a theoretical investigation and subsequent practical implementation of a ...
Dynamics of micro-air-vehicles with flapping wings: A multibody system approach
(Institute of Electrical and Electronics Engineers, 2013)
Aerodinámica del vuelo a números de Reynolds ultrabajos (Re<10000)
(2013)
El régimen de vuelo para los MAV (por Micro Air Vehicles), de por si plantea numerosos desafíos para el análisis y el diseño aerodinámico. Además, existen escasos experimentos computacionales para superficies aerodinámicas ...
Computational dynamics of flapping wings in hover flight: A co-simulation strategy
(Amer Inst Aeronaut Astronaut, 2017-06)
A co-simulation strategy for modeling the unsteady dynamics of flying insects and small birds as well as biologically inspired flapping-wing micro-air-vehicles is developed in this work. In particular, the dynamic system ...
Quadrotor Flight in Constrained Indoor Environments
(Instituto Nacional de Astrofísica, Óptica y Electrónica, 2020)
Towards bio-inspiration, development, and manufacturing of a flapping-wing micro air vehicle
(2020-09-01)
Throughout the last decade, there has been an increased demand for intricate flapping-wing drones with different capabilities than larger drones. The design of flapping-wing drones is focused on endurance and stability, ...
Piezoaeroelastic Modeling and Analysis of a Generator Wing with Continuous and Segmented Electrodes
(SAGE PUBLICATIONS LTD, 2010)
Unmanned air vehicles (UAVs) and micro air vehicles (MAVs) constitute unique application platforms for vibration-based energy harvesting. Generating usable electrical energy during their mission has the important practical ...
Comparative study on analytical and computational aerodynamic models for flapping wings MAVs
(Royal Aeronautical Soc, 2020-07)
A range of quasi-steady and unsteady aerodynamic models are used to predict the aerodynamic forces experienced by a flapping wing and a detailed comparison amongst these predictions in provided. The complexity of the models ...