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Methods and systems for operating a gas turbine engine system include an electrical generator configured to provide electrical energy to a load, a gas turbine engine including at least one combustor that includes a plurality of fuel injection points configured to inject a fuel into the combustor at

Methods and systems for operating a gas turbine engine system include an electrical generator configured to provide electrical energy to a load, a gas turbine engine including at least one combustor that includes a plurality of fuel injection points configured to inject a fuel into the combustor at a plurality of different locations wherein the combustor configured to combust the fuel and the gas turbine engine is rotatably coupled to the generator through a shaft. The gas turbine engine system includes a control system including a plurality of sensors positioned about the gas turbine engine system and configured to measure at least one parameter associated with the sensor, a processor programmed to receive a signal indicative of a heating value of the fuel, and automatically control a fuel split between the fuel injection points on the combustor using the determined heating value.

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What is claimed is: 1. A method of operating a gas turbine engine comprising: determining a heating value of the fuel; providing a combustor including a plurality of fuel injection points to combust the fuel; and automatically controlling a fuel split between the fuel injection points on the combus

What is claimed is: 1. A method of operating a gas turbine engine comprising: determining a heating value of the fuel; providing a combustor including a plurality of fuel injection points to combust the fuel; and automatically controlling a fuel split between the fuel injection points on the combustor using the determined heating value, wherein automatically controlling a fuel split between fuel injection points comprises: determining a first fuel split setting at a first heating value of the fuel; determining a second fuel split setting at a second heating value of the fuel; determining a fuel split using the determined first and second fuel split settings; and applying the determined fuel split to control fuel flow to the combustor. 2. A method in accordance with claim 1 wherein the heating value is represented by a Modified Wobbe Index (MWI) of the fuel. 3. A method in accordance with claim 2 wherein the Modified Wobbe index of the fuel is determined using: MWI represents the Modified Wobbe Index, LHV represents the fuel lower heating value, (Btu/scf), SGgas represents the specific gravity of the fuel gas with respect to air, and Tgas represents the fuel gas temperature in degrees Rankine. 4. A method in accordance with claim 1 wherein determining a fuel split using the determined first and second fuel split settings comprises at least one of interpolating between the determined first and second fuel split settings using the determined heating value of the fuel and extrapolating beyond the determined first and second fuel split settings using the determined heating value of the fuel. 5. A method in accordance with claim 1 wherein applying the determined fuel split to control fuel flow to the combustor comprises modifying a fuel split schedule for at least one combustor. 6. A method in accordance with claim 1 wherein the gas turbine engine is coupled to a fuel gas preheating system, said method further comprising transmitting to the fuel gas preheating system, a demand signal that modifies a fuel gas temperature. 7. A method of operating a gas turbine engine comprising: determining a first fuel split setting at a first fuel parameter value; modifying the first fuel parameter value to a second fuel parameter value by changing a temperature of the fuel from a first temperature value to a second temperature value wherein the second temperature value is different from the first temperature value; determining a second fuel split setting at the second fuel parameter value; determining a fuel split schedule using the determined first and second fuel split settings; and applying the determined fuel split schedule to control fuel flow to a combustor. 8. A method in accordance with claim 7 wherein the combustor includes a plurality of fuel injection points and wherein applying the determined fuel split schedule to control fuel flow to a combustor comprises controlling a proportion of fuel that is injected into each injection point such that the fuel parameter value is changed. 9. A method in accordance with claim 7 wherein determining a fuel split schedule comprises determining the fuel split schedule in real-time while the gas turbine engine is supplying electrical energy to an electrical load. 10. A method in accordance with claim 7 wherein the fuel parameter is represented by a Modified Wobbe Index (MWI) of the fuel. 11. A method in accordance with claim 10 wherein the Modified Wobbe Index of the fuel is determined using: MWI represents the Modified Wobbe Index, LIIV represents the fuel lower heating value, (Btu/scf), SGgas represents the specific gravity of the fuel gas with respect to air, and Tgas represents the fuel gas temperature in degrees Rankine. 12. A method in accordance with claim 7 wherein determining a fuel split schedule using the determined first and second fuel split settings comprises at least one of interpolating between the determined first and second fuel split settings using the determined fuel parameter values and extrapolating beyond the determined first and second fuel split settings using the determined fuel parameter values. 13. A method in accordance with claim 7 further comprising: coupling a fuel gas preheating system to the gas turbine engine; and transmitting a demand signal that modified a fuel gas temperature to the fuel gas preheating system.