Model Based Automatic Control Design for the T-FLEX Demonstrator Using RCE Environment

von Takarics, Béla
Veröffentlicht in AIAA SciTech Forum (2023 : National Harbor, Md.; Online) Structural dynamics ; Volume 1 of 3 (2023)

Aeroservoelastic Induced Drag Modelling and Minimization for the T-FLEX Demonstrator

von Meddaikar, Yasser M.
Veröffentlicht in AIAA SciTech Forum (2023 : National Harbor, Md.; Online) Structural dynamics ; Volume 1 of 3 (2023)

Flight Vibration Testing of the T-FLEX UAV Using Online Modal Analysis

von Soal, Keith
Veröffentlicht in AIAA SciTech Forum (2023 : National Harbor, Md.; Online) Structural dynamics ; Volume 1 of 3 (2023)

ACTIVE FLUTTER MITIGATION TESTING ON THE FLEXOP DEMONSTRATOR AIRCRAFT

von Takarics, Béla
Veröffentlicht in AIAA SciTech Forum and Exposition (2020 : Orlando, Fla.) Atmospheric flight mechanics ; Volume 2 of 2 (2020)

RESULTS OF AN AEROELASTICALLY TAILORED WING ON THE FLEXOP DEMONSTRATOR AIRCRAFT

von Roessler, Christian
Veröffentlicht in AIAA SciTech Forum and Exposition (2020 : Orlando, Fla.) Atmospheric flight mechanics ; Volume 2 of 2 (2020)

GROUND TESTING OF THE FLEXOP DEMONSTRATOR AIRCRAFT

von Sodja, Jurij
Veröffentlicht in AIAA SciTech Forum and Exposition (2020 : Orlando, Fla.) Atmospheric flight mechanics ; Volume 2 of 2 (2020)