A maximum output creator for a gas turbine which includes a compressor that compresses air to generate compressed air, a combustor that combusts fuel in the compressed air to generate combustion gas, and a turbine to be driven by the combustion gas, and in which the compressor includes an intake air amount regulator that regulates a flow rate of the air suctioned by the compressor, the creator comprising:
- a temperature reception unit that receives an intake air temperature which is a temperature of the air suctioned by the compressor;
- a change reception unit that receives a change content of a maximum opening degree of the intake air amount regulator;
- a basic maximum output computation unit that obtains a basic maximum output of the gas turbine based on the intake air temperature received by the temperature reception unit;
- a coefficient creation unit that creates a maximum output correction coefficient for correcting the basic maximum output based on the change content of the maximum opening degree received by the change reception unit and on the intake air temperature received by the temperature reception unit;
- and
- a maximum output correction unit that corrects the basic maximum output using the maximum output correction coefficient, and that outputs the corrected basic maximum output as a maximum output for control.