Flight Vibration Testing of the T-FLEX UAV using Online Modal Analysis-Reference-Cited by-同舟云学术

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

Published:2023-01-19 Issue: Volume: Page:
ISSN:
Container-title:AIAA SCITECH 2023 Forum
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Author:

Soal Keith¹,Volkmar Robin¹,Thiem Carsten¹,Sinske Julian¹,Meddaikar Yasser M.¹,Govers Yves¹,Böswald Marc¹,Teubl Daniel²,Bartasevicius Julius²,Nagy Mihaly³,Vanek Balint³

Affiliation:

1. Deutsches Zentrum fur Luft- und Raumfahrt eV

2. Technische Universitat Munchen

3. Eotvos Lorand Kutatasi Halozat Szamitastechnikai es Automatizalasi Kutatointezet

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2023-0373

Reference11 articles.

1. HALO flight test with instrumented under-wing stores for aeroelastic and load measurements in the DLR project iLOADS

2. The X-53 A Summary of the Active Aeroelastic Wing Flight Research Program

3. Design and flight test of active flutter suppression on the X-56A multi-utility technology test-bed aircraft

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