SENSOR FUSION OF STRUCTURAL FINITE ELEMENT MODEL WITH INERTIAL SENSOR DATA TO MEASURE WING DEFLECTION OF A FIXED WING AIRCRAFT

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Veröffentlicht in:AIAA SciTech Forum and Exposition (2020 : Orlando, Fla.) Sensor systems and information fusion
1. Verfasser: Schirmer, Georg (VerfasserIn)
Weitere Verfasser: Steck, James E. (VerfasserIn)
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Sprache:eng
Veröffentlicht: 2020
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