There is provided a system (100) and method for controlling an engine (10). A request signal indicative of a demand for the engine (10) to output a required power level is first received. A position control signal is then generated in response to the reque...

The present application thus provides a gas turbine engine system (100). The gas turbine engine system (100) may include a gas turbine engine (110), a nitrogen oxides reduction system (200) in communication with a flow of combustion gases (160) downstream ...

Certain embodiments of the invention may include systems, methods, and apparatus for determining steady state conditions in a gas turbine. According to an example embodiment of the invention, a method for determining stability in a gas turbine is provided....