HIGHLIGHTS
- who: Mohamed A. A. Ismail and collaborators from the (UNIVERSITY) have published the Article: Spall Fault Quantification Method for Flight Control Electromechanical Actuator, in the Journal: Actuators 2022, 11, x FOR PEER REVIEW of /2022/
- what: In this study a vibration-based quantification method is developed to quantify the fatigue faults of a ball-screw mechanism of an EMA. In this paper, a method was developed based on a first-time derivative of the vibration acceleration response, or the vibration jerk.
SUMMARY
There are many growing civil and military applications for . . .
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