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Sample Category

Revealing adverse rotorcraft pilot couplings induced by flight control system

  • Status: Active
  • Since November 2018

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NITROS project

ARISTOTEL project

About us

Our research concentrates on establishing a rational and systematic framework for physics-based modelling and simulation at rotorcraft applicable to the practices and processes involved in flight dynamics modelling, flight simulator development and handling qualities.The models we develop are according to the application considered and to the required level of fidelity.

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2629 HS Delft


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