Abstract
Abstract Based on ARINC 624 for civil aircraft airborne maintenance system, the working modes and application forms of civil aircraft Flight Control System Built-in Test (BIT) design are given. The test principles and implementation methods of the civil aircraft Flight Control System Power-on BIT and Initiated BIT are analyzed in detail, and the overall functional architecture of the civil aircraft Flight Control System BIT is described. Taking the actuator as an example, the realization method of its return to service test is analyzed. Finally, the general characteristics of the BIT technology of the civil aircraft Flight Control System are summarized.
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