... due to the transient fuel flow change using the Runge–Kutta method. In this transient performance simulation, the turbine overshoot was predicted. aerospace computing aerospace engines aerospace propulsion aircraft control control engineering computing digital simulation gas turbines...

...) while showing a good level of adaptivity, readiness, precision, robustness, and stability. 20 09 2006 15 12 2006 gas turbine power stations multi-agent systems control engineering computing power station control power engineering computing MIMO systems blades shafts...

... gas turbines closed loop systems fission reactors computational fluid dynamics power engineering computing mechanical engineering computing control system synthesis control engineering computing power grids 2007 American Society of Mechanical Engineers ...