A wing deformation monitoring and analysis system includes at least one image sensor installed on a portion of the aircraft such that at least one wing of the aircraft is located in a field of view (FOV) of the at least one image sensor. The image sensor outputs at least one image signal representing a captured wing image of the at least one wing. An electronic deformation controller is configured to compare the captured wing image to a nominal wing image, determines a deformation of the at least one wing based on the comparison.
AIRCRAFT WING DEFORMATION MONITORING AND ANALYSIS SYSTEM
2017-09-14
Patent
Electronic Resource
English
IPC: | B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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