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  1. Control & Simulation
  2. Aircraft System Identification and Control
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  5. Pressure Output Feedback Control of Tollmien–Schlichting Waves in Falkner–Skan Boundary Layers

Publications

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Stretch

Pressure Output Feedback Control of Tollmien–Schlichting Waves in Falkner–Skan Boundary Layers

  • Journal Articles
  • Published in 2019

H.J. Tol, M. Kotsonis, C.C. De Visser, Pressure Output Feedback Control of Tollmien–Schlichting Waves in Falkner–Skan Boundary Layers, AIAA Journal 57:1538-1551, 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...

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  • 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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