Electric aircraft, power distribution system, power supply control method and computer storage medium

A power distribution system for an electric aircraft, the electric aircraft comprising a fuselage, a plurality of rotors provided at the fuselage, and rotor motors configured to drive the rotors, the rotor motors being divided into two parts, and the power distribution system comprising:

• a first battery pack;
• a second battery pack;
• a first isolation device;
• and
• a second isolation device, wherein:
• the first battery pack and the second battery pack are electrically connected to a first part of the rotor motors via the first isolation device to supply power to the first part of the rotor motors;
• the first battery pack and the second battery pack are electrically connected to a second part of the rotor motors via the second isolation device to supply power to the second part of the rotor motors;
• and
• when a power supply failure occurs in the power distribution system, the first isolation device and the second isolation device isolate a faulty line and reconstruct power supply lines.