Open- and closed-loop results of a strain-actuated active aeroelastic wing

Lin et al summarize open- and closed-loop tests for a strain-actuated active aeroelastic wing. The saturation limit of the piezoelectrics, the choice of performance metric or output sensor, and the changes in the dynamic response of the test article are the three major performance limitations.

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Bibliographische Detailangaben
Veröffentlicht in:	Journal of aircraft 1996-09, Vol.33 (5), p.987-994
Hauptverfasser:	Lin, Charrissa Y, Crawley, Edward F, Heeg, Jennifer
Format:	Artikel
Sprache:	eng
Schlagworte:	Aerodynamics Avionics Exact sciences and technology Fundamental areas of phenomenology (including applications) Physics Solid mechanics Structural and continuum mechanics Vibration, mechanical wave, dynamic stability (aeroelasticity, vibration control...) Vibrations and mechanical waves
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Beschreibung
Zusammenfassung:	Lin et al summarize open- and closed-loop tests for a strain-actuated active aeroelastic wing. The saturation limit of the piezoelectrics, the choice of performance metric or output sensor, and the changes in the dynamic response of the test article are the three major performance limitations.
ISSN:	0021-8669 1533-3868
DOI:	10.2514/3.47045