| 摘要 |
PURPOSE: A power automatic control and distribution, and a method for protecting aircraft system are provided to automatically control and distribute AC(Alternating Current) and DC(Direct Current) control. CONSTITUTION: A power state of a board, an input port state of separated parts, an operation state of an analog board, and an operation state of a contactor are tested(S20). Power state of the EMB(Electrical Master Box) and a state by a switch input are monitored(S50). If a reset switch of EMB is activated, the defective state is set as a normal state(S60). If the monitoring state is normal state, a network reconfiguration and protection function are operated(S120).
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