Configurable aircraft power system

摘要

An aircraft power system includes a secondary power distribution assembly (SPDA), a programmable solid state power controller (SSPC) disposed within the SPDA and a non-volatile memory disposed within the SPDA and adapted to store configuration information for the programmable SSPC. The configuration information stored by the non-volatile memory may include the name and current rating of the SSPC and whether that SSPC is enabled or disabled.