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The process adopted for continuous monitoring of eigenfrequencies and damping ratios during the test flight of a research aircraft is presented. This comprises measurement hardware, distributed data acquisition system and software architecture in ord
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::cab33532921118d7d1bb1ab791dbdb23
https://doi.org/10.2514/6.2017-1825
https://doi.org/10.2514/6.2017-1825
Autor:
Julian Springer, Jan Schwochow, Marc Böswald, Julian Sinske, G. Jelicic, Ralf Buchbach, Yves Govers
Publikováno v:
Scopus-Elsevier
University of Southern Denmark
University of Southern Denmark
The work presented in this paper shows a simple way how to obtain eigenfrequencies, damping ratios and mode shapes of an aircraft prototype. The only prerequisite is flight test instrumentation (FTI) including a set of acceleration sensors with suffi
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::763434993003304052f9ad028ec3afa4
https://elib.dlr.de/115585/
https://elib.dlr.de/115585/