Multi-source electric energy control method and architecture

The invention discloses a multi-source electric energy control method and architecture, and belongs to the technical field of electromechanical equipment power supply. The multi-source electric energy control method comprises the following steps: S10, judging whether an aircraft is in a ground state or not; s20, judging whether the aircraft is in an emergency state or not; s30, whether the ram air turbine is discharged or not is judged; s40, Plt is judged; whether [alpha] Pe is established; s50, the SOClt is judged; whether SOCMAX is established or not; s60, Plt is judged; whether Pe is true or not; s70, Plt is judged; whether Pe + Pc is established; s80, the SOCgt is judged; whether SOCMIN is established or not; an architecture for performing a multi-source power control method includes a main generator, an energy storage device, a ram air turbine generator, a solid state power controller, a bus bar, and an electrical device. The problems that a power system energy architecture control method is single, and