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A method for reducing or eliminating oscillations in a gas turbine fuel control system includes utilizing an engine model to regulate a gas supply pressure for a gas turbine, sensing the pressure of gas actually supplied, and applying integral state feedback plus gas supply pressure feedforward comb

A method for reducing or eliminating oscillations in a gas turbine fuel control system includes utilizing an engine model to regulate a gas supply pressure for a gas turbine, sensing the pressure of gas actually supplied, and applying integral state feedback plus gas supply pressure feedforward combined with integral plus state feedback to the engine model to control and reduce gas fuel supply variations.

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What is claimed is: 1. A method for reducing or eliminating oscillations in a gas turbine fuel control system, said method comprising utilizing an engine model to regulate a gas supply pressure for a gas turbine; sensing the pressure of gas actually supplied; adding a pressure feedback signal from

What is claimed is: 1. A method for reducing or eliminating oscillations in a gas turbine fuel control system, said method comprising utilizing an engine model to regulate a gas supply pressure for a gas turbine; sensing the pressure of gas actually supplied; adding a pressure feedback signal from the engine model multiplied by a control gain to an integral signal to create a integral/sum signal; and applying integral state feedback plus gas supply pressure feedforward combined with integral plus state feedback to the engine model to control and reduce gas fuel supply variations. 2. A method in accordance with claim 1 wherein said adding a pressure feedback signal from the engine model multiplied by a control gain to an integral signal to create a integral/sum signal further comprises integrating a signal comprising a pressure feedback signal from the engine model subtracted from a pressure setpoint to create the integral signal. 3. A method in accordance with claim 2 wherein said applying integral state feedback plus gas supply pressure feedforward combined with integral plus state feedback to the engine model further comprises adding the pressure setpoint multiplied by a feed forward gain to the integral/sum signal to produce a feedforward/integral/sum signal. 4. A method in accordance with claim 2 wherein said applying integral state feedback plus gas supply pressure feedforward combined with integral plus state feedback to the engine model further comprises adding a measured gas supply pressure multiplied by a disturbance gain to the integral/sum signal to produce a disturbance/integral/sum signal. 5. A method in accordance with claim 4 wherein said applying integral state feedback plus gas supply pressure feedforward combined with integral plus state feedback to the engine model further comprises adding the pressure setpoint multiplied by a feed forward gain and a measured gas supply pressure multiplied by a disturbance gain to the integral/sum signal to produce a positive feedback reference signal input to the engine model. 6. An apparatus for reducing or eliminating oscillations in a gas turbine fuel control system, said apparatus comprising: an engine model component configured to regulate a gas supply pressure for a gas turbine; a pressure sensor configured to sense a pressure of gas actually supplied to the integral plus state feedback module comprising an addition module configured to: add a pressure feedback signal from the engine model multiplied by a control gain to an integral signal to create an integral/sum signal; and provide the integral/sum signal to the engine model to control and reduce gas fuel supply variations. 7. An apparatus in accordance with claim 6 wherein said integral state feedback plus gas supply pressure feedforward combined with integral plus state feedback module further comprises an integrator configured to integrate a signal comprising a pressure feedback signal from the engine model subtracted from a pressure setpoint to create the integral signal. 8. An apparatus in accordance with claim 7 wherein said integral state feedback plus gas supply pressure feedforward combined with integral plus state feedback module further comprises an addition module configured to add the pressure setpoint multiplied by a feed forward gain to the integral/sum signal to produce a feedforward/integral/sum signal. 9. An apparatus in accordance with claim 7 wherein said integral state feedback plus gas supply pressure feedforward combined with integral plus state feedback module further comprises an addition module configured to add a measured gas supply pressure multiplied by a disturbance gain to the integral/sum signal to produce a disturbance/integral/sum signal. 10. An apparatus in accordance with claim 9 wherein said addition module configured to add a measured gas supply pressure multiplied by a disturbance gain to the integral/sum signal is further configured to add the pressure setpoint multiplied by a feed forward gain and a measured gas supply pressure multiplied by a disturbance gain to the integral/sum signal to produce a positive feedback reference signal input to the engine model. 11. An apparatus in accordance with claim 6 further comprising a gas fuel supply controlled by the engine model and also further comprising a gas turbine.