FIELD: gas industry.
SUBSTANCE: created is a controller (600) 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 (600) is configured, in response to a load change 
L for the load L, to control the compressor (101) so as to provide air to the combustion chamber (102) with a new mass flow rate 
of air, wherein the new mass flow rate of air is within the range between the first threshold value 
and the second threshold value 
.
EFFECT: invention ensures control of a gas turbine.
13 cl, 17 dwg
