Aircraft universal power converter

A control system for a power supply comprising:

• a first controller configured to control an interleaved buck converter;
• a second controller configured to control an interleaved full-bridge converter;
• a third controller configured to control an interleaved inverter;
• and
• a supervisory controller configured to control operation of the first, second, and third controllers in response to a plurality of control signals.

A method for generating a plurality of regulated supply voltages, the method comprising:

• generating regulated low-voltage DC using power provided by a DC power source, wherein the regulated low-voltage DC is generated using an interleaved buck converter, and the DC power source is an unregulated DC power source;
• generating regulated high-voltage AC using power provided by the DC power source, wherein the regulated high-voltage AC is generated using an interleaved inverter;
• generating regulated high-voltage DC using power provided by the DC power source, wherein the regulated high-voltage DC is generated using an interleaved full-bridge converter;
• and
• controlling the interleaved buck converter, the interleaved full-bridge converter, and the interleaved inverter in response to a plurality of system control signals.