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Tytuł artykułu

Experimental study and neural network modelling of aerodynamic and dynamic characteristics of flapping wings micro aerial vehicle

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Języki publikacji
EN
Abstrakty
EN
The article is close connected with building flying object, that fly like an insect (entomopter). Present work concerns on concept of aerodynamic model using artificial neural networks. Model is used in simulations of flight of entomopter. Aerodynamic model based on experimental data. Necessary data are taken from experiment performed in water tunnel on entomopter model. For this case dynamic test are required. Measurements are ducted during sinusoidal motion of whole model. Modelled object is dipterous. Each wing can perform various spherical motions (wing is rotated around point). The motion of the wing in this case was two-dimensional; it was rotated around two axis. As a model, specially trained neural network is used. For training are used data from measurement. Presented in this article approach is based on artificial neural networks. In this article, innovative concept of model, describing unsteady aerodynamics of entomopter was proposed. It was shown that it could be easily implemented as mathematical model. Unsteady effects related to many state variables can be easily captured. Model can be easily adopted to predict different states of flight by networks training on appropriate data. Test has to reproduce real conditions as close, as it is possible. In reality, it is challenging to design test that will reproduce similar motion.
Twórcy
  • Institute of Aviation Krakowska Av. 110/114, Warszawa, Poland
autor
  • Air Force Institute of Technology Ks. Bolesława Street 6, 01-494 Warszawa, Poland
autor
  • Air Force Institute of Technology Ks. Bolesława Street 6, 01-494 Warszawa, Poland
Bibliografia
  • [1] Czekałowsk, P., Sibilski, K., Influence of Cruise Flight Speed of Entomopter on Aerodynamics Loads, AIAA online proceedings AIAA 2013-0770, 2013.
  • [2] Lasek, M., Sibilski, K., Modelling and Simulation of Flapping Wing Control for a Micromechanical Flying Insect, AIAA online proceedings AIAA 2002-4973, 2002.
  • [3] Lasek, M., Pietrucha, J., Sibilski, K., Złocka., Modelowanie dynamiki lotu ornitoptera, Warsaw University of Technology Report of project, Nr 9 T12C 004 18, 2003.
  • [4] Schenato, L., Analysis and Control of Flapping Flight:from Biological to Robotic Insects, Dissertation, University of Padua, 1999.
  • [5] Ansari, S. A., Żbikowski, R., Knowles, K., Aerodynamic modelling of Insect-like Flapping Flight for Micro Air Vehicles, Progres in Aerospace Sciences, Vol. 42. pp. 129-172, 2006.
  • [6] Shyy, W., Lian, Y., Tang, J., Vheru, D., Liu, H., Aerodynamics of low Reynolds number flyers, Cambridge University Press, ISBN 978-0-521, 2008.
  • [7] Ol, M. V., Unsteady Aerodynamics for Micro Air Vehicles, Report, AC/323(AVT-149)TP/332 ISBN 978-92-837-0118-7, 2010.
  • [8] Ol, M. V., Unsteady low Reynolds number aerodynamics for micro air vehicles (MAVs), AFRLRB-WP-TR-2010-3013, 2010.
  • [9] Jong-Seob Han, Jo Won Chang Flow, Visualization and Force Measurement of an Insect based Flapping Wing, AIAA online proceedings AIAA2010-66, 2010.
  • [10] Czekałowsk, P., Sibilski, K., Water tunnel experimental investigation on the aerodynamic performance of flapping wings for nano air vehicles, AIAA online proceedings AIAA 2010-3789, 2010.
  • [11] RHRC, Research water tunnel specification, El Segundo California 2009.
Uwagi
Opracowanie rekordu w ramach umowy 509/P-DUN/2018 ze środków MNiSW przeznaczonych na działalność upowszechniającą naukę (2018).
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-a8086433-985a-4dc6-a3db-ca679f59823b
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