A structural health monitoring system and method includes a plurality of sensors configured to collect sensed data, a first structural component, and a controller configured to receive the sensed data and detect a first condition based upon the sensed data. The controller is further configured to initiate a first structural interrogation of the first structural component upon detection of the condition.
AUTOMATED STRUCTURAL INTERROGATION OF AIRCRAFT COMPONENTS
2018-03-22
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 |
AUTOMATED STRUCTURAL INTERROGATION OF AIRCRAFT COMPONENTS
European Patent Office | 2018
|Aircraft Interrogation Scheduling with ASTRO-DABS
IEEE | 1974
|Aircraft distance measuring equipment with directional interrogation
European Patent Office | 2015
|REMOTE INTERROGATION AND OVERRIDE FOR AUTOMATED DRIVING SYSTEM
European Patent Office | 2017
|