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Titel:

Flight Testing for Flight Dynamics Estimation of Medium-Sized UAVs.

Dokumenttyp:
Konferenzbeitrag
Autor(en):
Koeberle, Sebastian J.; Albert, Adrian E.; Nagel, Lars H.; Hornung, Mirko
Abstract:
The Institute of Aircraft Design of Technical University of Munich designs, builds and tests Unmanned Aerial Vehicles (UAV) with take-off weights of up to 65~kg for the purpose of technology demonstration in flight. This purpose often leads to the incorporation of uncommon features. With growing size and unconventional features, the domain of validity of empiric design and analysis methods, often derived either from smaller UAVs or larger, manned aircraft, is left. Therefore a design-data based...     »
Kongress- / Buchtitel:
AIAA Scitech 2021 Forum
Verlag / Institution:
American Institute of Aeronautics and Astronautics
Publikationsdatum:
04.01.2021
Jahr:
2021
Print-ISBN:
9781624106095
Volltext / DOI:
doi:10.2514/6.2021-1526
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