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Modelling and Control of an Effort Feedback Actuator in Helicopter Flight Control Using Energetic Macroscopic Representation

Communication avec acte
Auteur
MARTIN, Mikael
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/10985/9780
Date
2011

Résumé

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. Their regulating loops are usually global PID controllers where parameters are directly set up on dedicated test benches. Energetic representation tools such as Energetic Macroscopic Representation (EMR) aim at simplifying systems analysis and control providing model and control structuring method. In this paper, a simplified helicopter flight axis control is modelled with the intention of controlling the helicopter stick force feedback. Performances of both global PID and energetic model based inversion controllers are discussed through simulation results.

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  • Laboratoire d’Ingénierie des Systèmes Physiques Et Numériques (LISPEN)

Documents liés

Visualiser des documents liés par titre, auteur, créateur et sujet.

  • Modelling and Control of a Complex Multi-physic System Application to Helicopter flight axis control 
    Communication avec acte
    MARTIN, Mikael; BARRE, Pierre-Jean; ccGOMAND, Julien; ccMALBURET, François (IEEE, 2012)
    A helicopter flight axis control, which is a complex multi-physic system, is modelled using an energetic based graphical tool. Element of the system are mainly composed of passive technologies and their number tends to ...
  • Multi-physic system simplification method applied to a helicopter flight axis active control 
    Communication avec acte
    MARTIN, Mikael; BARRE, Pierre-Jean; ccGOMAND, Julien; ccMALBURET, François (IEEE, 2012)
    A helicopter flight axis control, which is a complex multi-physic system, is modelled using an energetic based graphical tool: the Energetic Macroscopic Representation. Elements of the system are mainly composed of passive ...
  • 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 ...
  • Towards an Energetic Modeling of Rotorcraft Using Bond-Graphs 
    Communication avec acte
    CHIKHAOUI, Zeineb; PAVEL, Marilena; BARRE, Pierre-Jean; ccGOMAND, Julien; ccMALBURET, François (American Helicopter Society (AHS) International, 2013)
    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. ...

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