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Towards an Energetic Modeling of Rotorcraft Using Bond-Graphs

Communication avec acte
Auteur
CHIKHAOUI, Zeineb
PAVEL, Marilena
BARRE, Pierre-Jean
ccGOMAND, Julien
178374 Laboratoire des Sciences de l'Information et des Systèmes : Ingénierie Numérique des Systèmes Mécaniques [LSIS- INSM]
ccMALBURET, François

URI
http://hdl.handle.net/10985/9779
Date
2013

Résumé

The paper presents an energetic method of helicopters dynamics analysis to study the air resonance (AR) phenomena. First, a brief state of art of AR phenomena is presented and a simple energetic explanation is given. Then part of the state of art is devoted to the Bond Graph (BG) and Multi-Bond Graphs (MBG) modeling method showing several advantages of the tool and few examples of MBG researches applications. This work proposes a macroscopic energetic description of a helicopter through the Word Bond Graph representation. The MBG is then used for Rotor/fuselage structure modeling in order to study the AR phenomena instability. The MBG model results are presented and show the potential of the MBG method to predict such a complex phenomenon.

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Documents liés

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  • Understanding pilot biodynamical feedthrough coupling in helicopter adverse roll axis instability via lateral cyclic feedback control 
    Article dans une revue avec comité de lecture
    TOD, Georges; PAVEL, Marilena; BARRE, Pierre-Jean; ccGOMAND, Julien; ccMALBURET, François (Elsevier, 2016)
    The paper reassesses the mechanism of biodynamical feedthrough coupling to helicopter body motion in lateral-roll helicopter tasks. An analytical bio-aeroelastic pilot–vehicle model is first developed and tested for various ...
  • An upper limb musculoskeletal model using bond graphs for rotorcraft-pilot couplings analysis 
    Communication avec acte
    TOD, Georges; BARRE, Pierre-Jean; ccGOMAND, Julien; ccMALBURET, François (SIMBIO-M, 2014)
    Under certain flight conditions, a rotorcraft fuselage motions and vibrations might interact with its pilot voluntary and involuntary actions leading to potentially dangerous dynamic instabilities known as rotorcraft-pilot ...
  • Modelling and Control of an Effort Feedback Actuator in Helicopter Flight Control Using Energetic Macroscopic Representation 
    Communication avec acte
    MARTIN, Mikael; BARRE, Pierre-Jean; ccGOMAND, Julien; ccMALBURET, François (IMAACA 2011, 5th International Conference on Integrated Modeling and Analysis in Applied Control and Automation, 2011)
    In helicopter field, electromechanical devices controllers are usually designed and tuned from global analysis with transfer functions calculations. This leads to control architectures with a reduced number of controllers. ...
  • Modeling Stiffness and Damping in Rotational Degrees of Freedom Using Multibond Graphs 
    Communication avec acte
    TOD, Georges; BARRE, Pierre-Jean; ccGOMAND, Julien; ccMALBURET, François (2013)
    A contribution is proposed for the modeling of mechanical systems using multibond graphs. When modeling a physical system, it may be needed to catch the dynamic behavior contribution of the joints between bodies of the ...
  • An Energetic Approach to Aeroelastic Rotorcraft-Pilot Couplings Analysis 
    Communication avec acte
    TOD, Georges; BARRE, Pierre-Jean; BOUDON, Benjamin; ccGOMAND, Julien; ccMALBURET, François (2013)
    This paper describes an energetic method using multibond graphs to model multi-physical systems. Its potential in building physical meaningful graphs that represent equivalent mathematical models of classic analytical ...

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