The invention relates to an electrical generation method for supplying power to at least one
electrical network of an aircraft using an electrical generation
system, the aircraft comprising two power supply paths, each power supply path comprising an electrical converter and an electrical generator, the electrical
system comprising two regulation units (21a) respectively associated with each power supply path, each regulation unit (21a) comprising a correction module (5) comprising an integral corrector (CI), the method comprising steps consisting, for the correction module (5), in: determining a power
setpoint (PBP*), from a distribution
voltage setpoint (VDC*) and from a measurement of the distribution
voltage (VDC), determining a
divergence indicator (M3) from a gradient (GPBP*) of the power
setpoint (PBP*), and resetting the integral corrector (CI) of the regulation unit (21a) of the power supply path depending on the
divergence indicator (M3).