Computer-controlled production and post-overhaul testing of servo-actuators is already a fact. Some challenges still exist for performing similar testing on components installed in the aircraft.An implementation of such a scheme is presented, using state-of-the-art technology. The objective of the described technique is to perform diagnostic testing on flight control hardware sufficient to determine whether the component may be left on the aircraft.
Computer Aided Diagnostic Testing of Installed Flight Control Servo- Actuators
Sae Technical Papers
Aerospace Technology Conference and Exposition ; 1993
1993-09-01
Conference paper
English
Computer Aided Diagnostic Testing of Installed Flight Control Servo- Actuators
British Library Conference Proceedings | 1993
|TIBKAT | 1964
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