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A system and method for controlling the fuel flow rate in a direct metering fuel control system to compensate for actuator flow. The system includes a fuel metering pump that supplies fuel to a fluid-operated actuator and to a gas turbine engine combustor and determines, using a generated model of t

A system and method for controlling the fuel flow rate in a direct metering fuel control system to compensate for actuator flow. The system includes a fuel metering pump that supplies fuel to a fluid-operated actuator and to a gas turbine engine combustor and determines, using a generated model of the fuel metering pump and/or the fluid-operated actuator, fuel flow rate needed by the gas turbine engine and/or the actuator fuel flow rate needed by the fluid-operated actuator. The fuel flow rate of the fuel metering pump is controlled based on the determined actuator fuel flow rate and the determined engine fuel flow rate.

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1. A system for controlling fuel flow rate to a fluid-operated actuator and to a combustor in a gas turbine engine, comprising: a fuel metering pump coupled to receive fuel, and further coupled to receive a pump command representative of a desired fuel flow rate, the fuel metering pump operable, upo

1. A system for controlling fuel flow rate to a fluid-operated actuator and to a combustor in a gas turbine engine, comprising: a fuel metering pump coupled to receive fuel, and further coupled to receive a pump command representative of a desired fuel flow rate, the fuel metering pump operable, upon receipt of the pump command, to supply fuel at the desired fuel flow rate;a control unit including a control law and a state estimator, the state estimator comprising a software model of the fuel metering pump and an software model of the fluid-operated actuator,wherein: the state estimator coupled to receive an engine fuel flow rate command and an actuator position command and operable to supply state estimates of the fuel metering pump and the fluid-operated actuator, andthe control law is coupled to receive the engine fuel flow rate command, the actuator position command, and the state estimates, and is configured, in response to the engine fuel flow rate command, the actuator position command, and the state estimates, to supply the pump command to the fuel metering pump and an actuator control command to the fluid-operated actuator. 2. The system of claim 1, wherein the control unit: includes an engine model of the gas turbine engine; anddetermines, using the pump model, the actuator model, and the engine model, the engine fuel flow rate needed by the combustor and the actuator fuel flow rate needed by the fluid-powered actuator. 3. The system of claim 1, further comprising the fluid-operated actuator, and wherein the fluid-powered actuator comprises: an actuator coupled to selectively receive fuel at the actuator fuel flow rate and operable, upon receipt thereof, to supply an actuation drive force; anda servo valve coupled to receive fuel supplied by the fuel metering pump, the servo valve further coupled to receive the actuator control command and operable, upon receipt thereof, to selectively supply the received fuel, at the actuator fuel flow rate, to the actuator. 4. The system of claim 1, wherein the fuel metering pump comprises: a positive displacement pump having an inlet and an outlet, the inlet adapted to receive fuel, the positive displacement pump coupled to receive a drive force and operable, upon receipt thereof, to supply fuel via the outlet;an electric motor coupled to the positive displacement pump and adapted to receive electrical current, the electric motor configured, upon receipt of the electrical current, to supply the drive force to the positive displacement pump; anda pump controller coupled to receive the pump command and operable, in response thereto, to control the electrical current supplied to the electric motor such that the drive force supplied by the electric motor causes the positive displacement pump to supply fuel at the desired fuel flow rate. 5. The system of claim 1, wherein the fuel metering pump comprises: a variable displacement pump having an inlet, an outlet, the inlet adapted to receive fuel, the variable displacement pump coupled to receive a drive force and operable, upon receipt thereof, to supply fuel via the outlet;a pump controller coupled to receive the pump command and operable, in response thereto, to supply actuator control signals; anda pump displacement control actuator coupled to the variable displacement pump and further coupled to receive the actuator control signals, the pump displacement control actuator configured, upon receipt of the actuator control signals, to control the displacement of the variable displacement pump such that the variable displacement pump supplies fuel at the desired fuel flow rate. 6. A system for controlling fuel flow rate to a fluid-operated actuator and to a combustor in a gas turbine engine, comprising: a fuel metering pump coupled to receive fuel, and further coupled to receive a pump command representative of a desired fuel flow rate, the fuel metering pump operable, upon receipt of the pump command, to supply fuel at the desired fuel flow rate;a control unit having a pump model of the fuel metering pump and an actuator model of the fluid-operated actuator stored therein, wherein the pump model is a software model of the fuel metering pump and the actuator model is a software model of the fluid-operated actuator, the control unit configured to: (i) determine, using the pump model and the actuator model, engine fuel flow rate needed by the combustor and actuator fuel flow rate needed by the fluid-powered actuator,(ii) determine the desired fuel flow rate from the determined engine fuel flow rate and the determined actuator fuel flow rate, and(iv) supply the pump command to the fuel metering pump,wherein the fuel metering pump comprises: a positive displacement pump having an inlet and an outlet, the inlet adapted to receive fuel, the positive displacement pump coupled to receive a drive force and operable, upon receipt thereof, to supply fuel via the outlet,an electric motor coupled to the positive displacement pump and adapted to receive electrical current, the electric motor configured, upon receipt of the electrical current, to supply the drive force to the positive displacement pump, anda pump controller coupled to receive the pump command and operable, in response thereto, to control the electrical current supplied to the electric motor such that the drive force supplied by the electric motor causes the positive displacement pump to supply fuel at the desired fuel flow rate. 7. The system of claim 6, wherein: the pump model and the actuator model are each coupled to simultaneously receive an engine fuel flow rate command and an actuator position command, the actuator position command representative of a position to which the fluid-operated actuator is to be moved; andthe pump model and the actuator model determine the engine fuel flow rate and the actuator fuel flow rate based at least in part on the engine fuel flow rate command and the actuator position command. 8. The system of claim 7, wherein the control unit: includes an engine model of the gas turbine engine; anddetermines, using the pump model, the actuator model, and the engine model, the engine fuel flow rate needed by the combustor and the actuator fuel flow rate needed by the fluid-powered actuator. 9. The system of claim 7, wherein the control unit includes: a state estimator that comprises the pump model and the actuator model, the state estimator operable to supply state estimates of the fuel metering pump and the fluid-operated actuator; anda control law coupled to receive the engine fuel flow rate command, the actuator position command, and the state estimates, the control law configured, in response to the engine fuel flow rate command, the actuator position command, and the state estimates, to supply the pump command to the fuel metering pump and an actuator control command to the fluid-operated actuator. 10. The system of claim 9, further comprising the fluid-operated actuator, and wherein the fluid-powered actuator comprises: an actuator coupled to selectively receive fuel at the actuator fuel flow rate and operable, upon receipt thereof, to supply an actuation drive force; anda servo valve coupled to receive fuel supplied by the fuel metering pump, the servo valve further coupled to receive the actuator control command and operable, upon receipt thereof, to selectively supply the received fuel, at the actuator fuel flow rate, to the actuator. 11. The system of claim 10, wherein the control unit includes: an engine control law configured to selectively supply the engine fuel flow rate command and the actuator position commands. 12. The system of claim 10, further comprising: a priority valve disposed between the fuel metering pump and the fluid-operated actuator, the priority valve coupled to receive valve position commands and movable, in response to the valve position commands, between a closed position, in which the fluid-operated actuator is fluidly isolated from the fuel metering pump, and an open position, in which the fluid-operated actuator is in fluid communication with the fuel metering pump,wherein the control unit is further configured to: determine if the engine is undergoing an engine-start sequence,supply valve position commands to the priority valve that cause the priority valve to move to the closed position if the engine is undergoing the engine-start sequence, andsupply valve position commands to the priority valve that cause the priority valve to move to the open position if the engine is not undergoing the engine-start sequence. 13. A system for controlling fuel flow rate to a fluid-operated actuator and to a combustor in a gas turbine engine, comprising: a fuel metering pump coupled to receive fuel, and further coupled to receive a pump command representative of a desired fuel flow rate, the fuel metering pump operable, upon receipt of the pump command, to supply fuel at the desired fuel flow rate;a control unit having a pump model of the fuel metering pump and an actuator model of the fluid-operated actuator stored therein, wherein the pump model is a software model of the fuel metering pump and the actuator model is a software model of the fluid-operated actuator, the control unit configured to: (i) determine, using the pump model and the actuator model, engine fuel flow rate needed by the combustor and actuator fuel flow rate needed by the fluid-powered actuator,(ii) determine the desired fuel flow rate from the determined engine fuel flow rate and the determined actuator fuel flow rate, and(iv) supply the pump command to the fuel metering pump,wherein the fuel metering pump comprises: a variable displacement pump having an inlet, an outlet, the inlet adapted to receive fuel, the variable displacement pump coupled to receive a drive force and operable, upon receipt thereof, to supply fuel via the outlet,a pump controller coupled to receive the pump command and operable, in response thereto, to supply actuator control signals, anda pump displacement control actuator coupled to the variable displacement pump and further coupled to receive the actuator control signals, the pump displacement control actuator configured, upon receipt of the actuator control signals, to control the displacement of the variable displacement pump such that the variable displacement pump supplies fuel at the desired fuel flow rate. 14. The system of claim 13, wherein: the pump model and the actuator model are each coupled to simultaneously receive an engine fuel flow rate command and an actuator position command, the actuator position command representative of a position to which the fluid-operated actuator is to be moved; andthe pump model and the actuator model determine the engine fuel flow rate and the actuator fuel flow rate based at least in part on the engine fuel flow rate command and the actuator position command. 15. The system of claim 14, wherein the control unit: includes an engine model of the gas turbine engine; anddetermines, using the pump model, the actuator model, and the engine model, the engine fuel flow rate needed by the combustor and the actuator fuel flow rate needed by the fluid-powered actuator. 16. The system of claim 14, wherein the control unit includes: a state estimator that comprises the pump model and the actuator model, the state estimator operable to supply state estimates of the fuel metering pump and the fluid-operated actuator; anda control law coupled to receive the engine fuel flow rate command, the actuator position command, and the state estimates, the control law configured, in response to the engine fuel flow rate command, the actuator position command, and the state estimates, to supply the pump command to the fuel metering pump and an actuator control command to the fluid-operated actuator. 17. The system of claim 16, further comprising the fluid-operated actuator, and wherein the fluid-powered actuator comprises: an actuator coupled to selectively receive fuel at the actuator fuel flow rate and operable, upon receipt thereof, to supply an actuation drive force; anda servo valve coupled to receive fuel supplied by the fuel metering pump, the servo valve further coupled to receive the actuator control command and operable, upon receipt thereof, to selectively supply the received fuel, at the actuator fuel flow rate, to the actuator.