A wing deformation monitoring and analysis system includes at least one image sensor (02a, 102b) installed on a portion of the aircraft (100) such that at least one wing (110a, 110b) 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 (202) 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
SYSTEM ZUR ÜBERWACHUNG UND ANALYSE VON FLUGZEUGFLÜGELVERFORMUNGEN
SYSTÈME DE SURVEILLANCE ET D'ANALYSE DE DÉFORMATION D'AILE D'AÉRONEF
2019-12-04
Patent
Elektronische Ressource
Englisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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