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Modeling Stiffness and Damping in Rotational Degrees of Freedom Using Multibond Graphs

Communication avec acte
Auteur
TOD, Georges
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/10985/9227
Date
2013

Résumé

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 system and therefore to characterize the stiffness and damping of the links between them. The visibility of where dissipative or capacitive elements need to be implemented to represent stiffness and damping in multibond graphs is not obvious and will be explained. A multibond graph architecture is then proposed to add stiffness and damping in hree rotational degrees of freedom. The resulting joint combines the spherical joint multibond graph relaxed causal constraints while physically representing three concatenated revolute joints. The mathematical foundations are presented, and then illustrated through the modeling and simulation of an inertial navigation system; in which stiffness and damping between the gimbals are taken into account. This method is particularly useful when modeling and simulating multibody systems using Newton-Euler formalism in multibond graphs. Future work will show how this method can be extended to more complex systems such as rotorcraft blades' connections with its rotor hub.

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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 ...
  • 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 ...
  • Complementary use of BG and EMR formalisms for multiphysics systems analysis and control 
    Communication avec acte
    CHIKHAOUI, Zeineb; BARRE, Pierre-Jean; ccGOMAND, Julien; ccMALBURET, François (ASME, 2012)
    In this paper, a complex multiphysics system is modeled using two different energy-based graphical techniques: Bond Graph and Energetic Macroscopic Representation. These formalisms can be used together to analyze, model ...
  • 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. ...

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