In a brushless alternator, the __**Permanent Magnetic Field**__ is created by a set of magnets that are mounted on the rotor. As the rotor spins, the magnets create a magnetic field that passes over the stator windings, inducing an electrical current in them. This electrical current is typically small, but it is used to power the exciter field.
__**The Exciter Field**__ is a winding on the stator that is powered by the small electrical current generated by the permanent magnetic field. As current flows through the exciter field, it creates a magnetic field that passes over the rotor, inducing an electrical current (that is larger than the permanent magnet could make) in the __**Exciter Output**__ windings.
The __**Main Output Field**__ is the winding on the rotor that generates the majority of the electrical output of the alternator. It is connected to the exciter output through a set of diodes that rectify the AC Exciter output to DC, which is then used to power the main output field. The main output field creates a large magnetic field that induces a much larger electrical current in the __**Main Output Stator**__ windings than the permanent magnet could. This electrical current is the final output of the alternator and can be used to power aircraft electrical systems.
Overall, the combination of the permanent magnetic field, the exciter field, and the main output field creates a self-sustaining system that generates electrical power without the need for brushes or a commutator. The system is controlled by electronic voltage regulators that monitor the output and adjust the excitation current as necessary to maintain a stable supply of electrical power. The GCU is usually connected to the airplane's electrical system and may communicate with other avionics systems to provide data and status information.