FIELD: gas industry.
SUBSTANCE: proposed is a controller (700) for a gas turbine (100). The gas turbine (100) is comprised of a compressor (101) configured to operate at a rotational rate 
, a combustion chamber (102), and a fuel supply tool (127) containing a first fuel supply tool and a second fuel supply tool, wherein the compressor (101) configured to provide air to the combustion chamber (102) with a mass flow rate 
of air in a steady state, wherein the fuel supply tool (127) is configured to supply fuel with a mass flow rate 
of the fuel into the combustion chamber (102). The controller (700) is configured, in response to a load change 
L for the load L, to control the fuel supply tool so as to supply a proportion Z of the mass flow rate of the fuel as the mass flow rate 
of the fuel through the first fuel supply tool based at least partially on the mass flow rate 
in the combustion chamber.
EFFECT: invention ensures control of a gas turbine.
12 cl, 17 dwg
