CONTROL DEVICE FOR AIRCRAFT

When a first generator (46a) is stopped, an electric motor control section (90) reduces the output power of a VTOL electric motor (20V) and a cruise electric motor (24C) that operate with electric power supplied from the first generator (46a), and increases the output power of a VTOL electric motor (20V) and a cruise electric motor (24C) that operate with electric power supplied from a second generator (46b).