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  1. Control & Simulation
  2. Aircraft System Identification and Control
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  5. Modelling wing wake and tail aerodynamics of a flapping-wing micro aerial vehicle

Publications

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Stretch

Modelling wing wake and tail aerodynamics of a flapping-wing micro aerial vehicle

  • Journal Articles
  • Published in 2019

S.F. Armanini, J.V. Caetano, C.C. de Visser, M.D. Pavel, G. de Croon, M. Mulder, Modelling wing wake and tail aerodynamics of a flapping-wing micro aerial vehicle, International Journal of Micro Air Vehicles 11, 2019


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We strive to make aerospace applications safer and more efficient through the application of system identification and control theory!

Aircraft Stall Model Identification
Project

This project focuses on developing dynamic models of aircraft in the stall and post-stall regime from flight data obtain...

Read more

  • Cum Laude for Dr. Tigran Mkoyan
  • NWO-Vidi grant (800.00 euros) for dr. Coen de Visser
  • PhD Defense Dr. Sihao Sun
  • Incremental Control on IEEE Spectrum

Aircraft System Identification and Control
Kluyverweg 1
2629 HS Delft

c.c.devisser@tudelft.nl ?
+31 15 2785246

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