The invention relates to a method for adjusting a
turbine, characterized in that during a first step (E1), first points (Yp, Yv) of iso-power, first values of the first command (Yp) for blade orientation and first values of the second command (Yv) for the orientation of the gate guide vanes are determined for target electrical powers (P1, P2, ... Pn), during a second step (E2), first points (Yp, Yv) of iso-power are determined for each target electrical power (P1, P2, ... Pn) in each set (Y1, Y2, ... Yn) of first points (Yp, Yv) of iso-power, the first point (INF(Yp, Yv)) of iso-power having a
maximum slope break in absolute value, during a third step (E3), the optimum adjustment points (INF(Yp, Yv)) for the target electrical powers (P1, P2, ... Pn) are recorded.