Study of the Functional Test and Quality Assurance Procedure of High Performance Aircraft Control Surfaces Integrate Servo Actuator

고성능 통합 비행 조정면 구동 장치의 성능 시험 및 품질보증 절차 수립에 관한 연구

This report analyzes the Source Qualification Test which is composed of main functional and environmental tests for the localizing avionics(electronic subsystem for aircrafts and spacecraft) and high performance mechanical subsystem. Especially the detail test approaches of integrated servo actuators which is the main part to supply the power to the main and other flying control panel. Nowadays this subsystem works with mechanical and electrical engineering technique. In detail, electrical signal is used as input and transferring tool and mechanical part is the output as a power and manufacture the physical dimensions and functions. Finally in this review, the new test procedure to prove the function by the new manufacturer is established.