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A method of operating a turbocharged system includes controlling speed of a turbocharger and substantially eliminating choke of a compressor coupled to a turbine by adjusting exhaust flow through a turbine wastegate, or by adjusting airflow through a compressor recirculation valve, or by adjusting a

A method of operating a turbocharged system includes controlling speed of a turbocharger and substantially eliminating choke of a compressor coupled to a turbine by adjusting exhaust flow through a turbine wastegate, or by adjusting airflow through a compressor recirculation valve, or by adjusting a combination thereof in response to variance in parameters including compressor inlet temperature, compressor inlet pressure, and turbocharger speed.

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1. A method of operating a turbocharged system, comprising: controlling speed of a turbocharger and substantially eliminating choke of a compressor coupled to a turbine by adjusting exhaust flow through a turbine wastegate, or by adjusting airflow through a compressor recirculation valve, or by adju

1. A method of operating a turbocharged system, comprising: controlling speed of a turbocharger and substantially eliminating choke of a compressor coupled to a turbine by adjusting exhaust flow through a turbine wastegate, or by adjusting airflow through a compressor recirculation valve, or by adjusting a combination thereof in response to variance in parameters including compressor inlet temperature, compressor inlet pressure, and turbocharger speed;calculating a corrected turbocharger speed based on an actual turbocarger speed and the compressor inlet temperature; andretarding or advancing fuel injection timing if a maximum pressure within a combustion chamber is greater than or less than a preselected maximum pressure, respectively. 2. The method of claim 1, further comprising at least partially opening the turbine wastegate, or the compressor recirculation valve, or a combination thereof if the compressor inlet pressure is less than a preselected pressure and if the compressor inlet temperature is less than a preselected temperature and if the turbocharger speed is greater than a preselected speed. 3. The method of claim 1, further comprising at least partially closing the turbine wastegate, or the compressor recirculation valve, or a combination thereof if the compressor inlet pressure is less than a preselected pressure and if the compressor inlet temperature is less than a preselected temperature and if the turbocharger speed is less than a preselected speed. 4. A method of manufacturing a turbocharged system, comprising: providing a controller configured to control speed of a turbocharger and substantially eliminate choke of a compressor coupled to the turbine by adjusting airflow through a compressor recirculation valve in response to variance in parameters including compressor inlet temperature, compressor inlet pressure, and turbocharger speed;wherein the controller is configured to calcuulate a corrected turbocharger speed based on an actual turbocharger speed and the compressor inlet temperature; wherein the controller configured to at least partially open or close a turbine wastegate to adjust exhaust flow to the atmosphere rather than to the turbine as the compressor inlet temperature, the compressor inlet pressure, and the turbocharger speed vary relative to preselected values. 5. The method of claim 4, comprising providing the controller configured to control speed of the turbocharger and substantially eliminate choke of the compressor coupled to the turbine by adjusting exhaust flow through a turbine wastegate in response to variance in parameters including compressor inlet temperature, compressor inlet pressure, and turbocharger speed. 6. A method of operating a turbocharged system, comprising: controlling speed of a turbocharger and substantially eliminating choke of a compressor coupled to a turbine by adjusting exhaust flow through a turbine wastegate, or by adjusting airflow through a compressor recirculation valve, or by adjusting a combination thereof in response to variance in parameters including compressor inlet temperature, compressor inlet pressure, and turbocharger speed; wherein:if the compressor inlet pressure and the compressor inlet temperature are less than first preselected values, then controlling comprises:at least partially opening the turbine wastegate, or the compressor recirculation valve, or a combination thereof if the turbocharger speed is greater than a first preselected speed; orat least partially closing the turbine wastegate, or the compressor recirculation valve, or a combination thereof if the turbocharger speed is less than a second preselected speed; orif the compressor inlet pressure and the compressor inlet temperature are greater than second preselected values, then controlling comprises at least partially closing the turbine wastegate. 7. The method of claim 6, wherein adjusting exhaust flow comprises at least partially opening the turbine wastegate, or adjusting airflow comprises at least partially opening the compressor recirculation valve, or a combination thereof if the compressor inlet pressure is less than a preselected pressure and if the compressor inlet temperature is less than a preselected temperature and if the turbocharger speed is greater than a preselected speed. 8. The method of claim 6, wherein adjusting exhaust flow comprises at least partially closing the turbine wastegate, or adjusting airflow comprises at least partially opening the compressor recirculation valve, or a combination thereof if the compressor inlet pressure is less than a preselected pressure and if the compressor inlet temperature is less than a preselected temperature and if the turbocharger speed is less than a preselected speed. 9. The method of claim 6, comprising at least partially closing the turbine wastegate if the compressor inlet pressure is greater than a preselected pressure and if the compressor inlet temperature is greater than a preselected temperature. 10. The method of claim 6, comprising retarding fuel injection timing if a maximum pressure within a combustion chamber exceeds a preselected maximum pressure. 11. The method of claim 6, comprising advancing fuel injection timing if a maximum pressure within a combustion chamber is less than a preselected maximum pressure. 12. The method of claim 6. wherein controlling speed of the turbocharger and substantially eliminating choke of the compressor is performed by derating engine power. 13. The method of claim 6, wherein controlling speed of the turbocharger and substantially eliminating choke of the compressor comprises at least partially opening or closing the turbine wastegate to adjust exhaust flow to the atmosphere rather than the turbine as the compressor inlet temperature, the compressor inlet pressure, and the turbocharger speed vary relative to preselected values. 14. The method of claim 6, comprising retarding or advancing fuel injection timing if a maximum pressure within a combustion chamber is greater than or less than a preselected maximum pressure, respectively. 15. A system, comprising: a controller configured to control speed of a turbocharger and substantially eliminate choke of a compressor coupled to a turbine by adjusting airflow through a compressor recirculation valve in response to variance in parameters including compressor inlet temperature, compressor inlet pressure, and turbocharger speed;wherein the controller is configured to calculate a corrected turbocharger speed based on an actual turbocharger speed and the compressor inlet temperature; wherein the controller is configured to control speed of the turbocharger and substantially eliminate choke of the compressor coupled to the turbine by adjusting exhaust flow through a turbine wastegate in response to variance in parameters including compressor inlet temperature, compressor inlet pressure, and turbocharger speed. 16. The system of claim 15, wherein the controller is configured to at least partially open the turbine wastegate, or the compressor recirculation valve, or a combination thereof if the compressor inlet pressure is less than a preselected pressure and if the compressor inlet temperature is less than a preselected temperature and if the turbocharger speed is greater than a preselected speed. 17. The system of claim 15, wherein the controller is configured to at least partially close the turbine wastegate, or the compressor recirculation valve, or a combination thereof if the compressor inlet pressure is less than a preselected pressure and if the compressor inlet temperature is less than a preselected temperature and if the turbocharger speed is less than a preselected speed. 18. A system, comprising: a controller configured to control speed of a turbocharger and substantially eliminate choke of a compressor coupled to a turbine by adjusting exhaust flow through a turbine wastegate, or by adjusting airflow through a compressor recirculation valve, or by adjusting a combination thereof in response to variance in parameters including compressor inlet temperature, compressor inlet pressure, and turbocharger speed; andan intake manifold air temperature sensor, an intake manifold air pressure sensor, a fuel injection timing sensor, and a turbocharger speed sensor;wherein the controller is configured to calculate a corrected turbocharger speed based on an actual turbocharger speed and the compressor inlet temperature; wherein the controller is configured to determine a maximum pressure in a combustion chamber based on signals from the intake manifold air temperature sensor, or the intake manifold air pressure sensor, or the fuel injection timing sensor, or a combination thereof. 19. A computer-readable medium having a computer program comprising: code to control speed of a turbocharger and substantially eliminate choke of a compressor coupled to the turbine by adjusting exhaust flow through a turbine wastegate, or by adjusting airflow through a compressor recirculation valve, or by adjusting a combination thereof in response to variance in parameters including compressor inlet temperature, compressor inlet pressure, and turbocharger speed;wherein if the compressor inlet pressure is less than a preselected pressure and if the compressor inlet temperature is less than a preselected temperature, thenthe code is configured for at least partially opening the turbine wastegate, or the compressor recirculation valve, or a combination thereof, if the turbocharger speed is greater than a preselected speed; orthe code is configured for at least partially closing the turbine wastegate, or the compressor recirculation valve, or a combination thereof, if the turbocharger speed is less than a preselected speed. 20. The computer-readable medium of claim 19, wherein the code is configured for at least partially opening the turbine wastegate, or the compressor recirculation valve, or the combination thereof if the compressor inlet pressure is less than the preselected pressure and if the compressor inlet temperature is less than the preselected temperature and if the turbocharger speed is greater than the preselected speed. 21. The computer-readable medium of claim 19, wherein the code is configured for at least partially closing the turbine wastegate, or the compressor recirculation valve, or the combination thereof if the compressor inlet pressure is less than the preselected pressure and if the compressor inlet temperature is less than the preselected temperature and if the turbocharger speed is less than the preselected speed. 22. The computer-readable medium of claim 19, wherein the code is configured to at least partially open or close the turbine wastegate to adjust exhaust flow to the atmosphere rather than the turbine as the compressor inlet temperature, the compressor inlet pressure, and the turbocharger speed vary relative to preselected values. 23. The computer-readable medium of claim 19, wherein the code is configured for calculating a corrected turbocharger speed based on an actual turbocharger speed and the compressor inlet temperature. 24. A system, comprising: a controller configured to control speed of a turbocharger and substantially eliminate choke of a compressor coupled to a turbine by adjusting exhaust flow through a turbine wastegate, or by adjusting airflow through a compressor recirculation valve, or by adjusting a combination thereof in response to variance in parameters including compressor inlet temperature, compressor inlet pressure, and turbocharger speed; wherein:if the compressor inlet pressure and the compressor inlet temperature are less than first preselected values, then the controller is configured to:at least partially open the turbine wastegate, or the compressor recirculation valve, or a combination thereof if the turbocharger speed is greater than a first preselected speed; orat least partially close the turbine wastegate, or the compressor recirculation valve, or a combination thereof if the turbocharger speed is less than a second preselected speed; orif the compressor inlet pressure and the compressor inlet temperature are greater than second preselected values, then the controller is configured to at least partially close the turbine wastegate. 25. The system of claim 24, further comprising an inlet pressure sensor configured to detect the compressor inlet pressure and an inlet temperature sensor configured to detect the compressor inlet temperature. 26. The system of claim 24, wherein the controller is configured to calculate a corrected turbocharger speed based on an actual turbocharger speed and the compressor inlet temperature. 27. The system of claim 24, wherein the controller is configured to at least partially open the turbine wastegate, or the compressor recirculation valve, or a combination thereof if the compressor inlet pressure is less than a preselected pressure and if the compressor inlet temperature is less than a preselected temperature and if the turbocharger speed is greater than a preselected speed. 28. The system of claim 24, wherein the controller is configured to at least partially close the turbine wastegate, or the compressor recirculation valve, or a combination thereof if the compressor inlet pressure is less than a preselected pressure and if the compressor inlet temperature is less than a preselected temperature and if the turbocharger speed is less than a preselected speed. 29. The system of claim 24, further comprising an intake manifold air temperature sensor, an intake manifold air pressure sensor, a fuel injection timing sensor, and a turbocharger speed sensor. 30. The system of claim 29, wherein the controller is configured to determine a maximum pressure in a combustion chamber based on signals from the intake manifold air temperature sensor, or the intake manifold air pressure sensor, or the fuel injection timing sensor, or a combination thereof 31. The system of claim 30, wherein the controller is configured to retard fuel injection timing if the maximum pressure within the combustion chamber exceeds a preselected maximum pressure, and if fuel injection timing is greater than or equal to a predetermined injection timing limit. 32. The system of claim 31, wherein the controller is configured to advance fuel injection timing if the maximum pressure within the combustion chamber is less than a preselected maximum pressure, and if the fuel injection timing is less than the predetermined injection timing limit. 33. The system of claim 24, wherein the controller is configured to control engine speed. 34. The system of claim 24, comprising the turbocharger having the controller. 35. The system of claim 24, comprising a compression-ignition engine having the controller. 36. The system of claim 24, comprising a locomotive having the controller coupled to an engine. 37. The system of claim 24, comprising an automobile having the controller coupled to an engine. 38. The system of claim 24, wherein the controller is configured to at least partially open or close the turbine wastegate to adjust exhaust flow to the atmosphere rather than the turbine as the compressor inlet temperature, the compressor inlet pressure, and the turbocharger speed vary relative to preselected values. 39. The system of claim 24, wherein the controller is configured to retard or advance fuel injection timing if a maximum pressure within a combustion chamber is greater than or less than a preselected maximum pressure, respectively.