Power supply and distribution reconfigurable control system and method oriented to batch flight verifications

The invention relates to a power supply and distribution reconfigurable control system and method oriented to batch flight verifications. Aiming at the problems of the failure and dynamic power demandchange of a power supply and distribution unit in the process of in-orbit batch flight verification of a future component, the cross recombination output control of power supply and distribution output is implemented on a power supply and distribution output terminal by using four groups of magnetic latching relays; and in the process of an aerospace in-orbit flight test, the in-orbit dynamic reconfiguration for the power supply output control of the power supply and distribution unit can be implemented through cross recombination according to the dynamic power requirement of a test unit andthe task fault-tolerant control need. With the power supply and distribution reconfigurable control system and method oriented to the batch flight verification disclosed by the invention, the flexibility and expansibility of t