The invention relates to a burner (10) for a gas turbine having a fuel supply device (20, 34, 44) for supplying fuel into the burner (10), which burner (10) is configured for mixing the fuel with an oxygen containing gas to generate a combustion medium to be supplied to a combustion chamber of the gas turbine. According to the invention said burner (10) is provided with a pressure measurement device (20) for pressure measurement in the combustion medium and comprising a measuring point (28) defining the location of the pressure measurement, wherein the measuring point (28) is located inside the burner (10), and the burner (10) is provided with a control device (64) configured for controlling the fuel supply of the fuel supply device (20, 34, 44) based on the pressure measurement and/or configured for controlling the air supply to the burner (10) based on the pressure measurement.
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