... engines aircraft control closed loop systems dynamic response Kalman filters mean square error methods open loop systems optimisation self-adjusting systems state estimation 25 04 2011 28 04 2011 27 01 2012 27 01 2012 2012 American Society of Mechanical Engineers ...

... a Stall Margin Control Mode ,” ASME J. Eng. Gas Turbines Power , 132 ( 5 ), p. 051602 . 25 04 2011 03 05 2011 07 11 2011 07 11 2011 aircraft control compressors correlation methods gas turbines rotors stability The control systems for aircraft gas turbine...

... and Automation , Haifa, Israel, pp. 593 – 602 . Wang , J. , and Sundararajan , N. , 1995 , “ A Nonlinear Flight Controller Design for Aircraft ,” Control Eng. Pract. 0967-0661 , 3 ( 6 ), pp. 813 – 825 . 10.1016/0967-0661(95)00064-2 Wang , J. , and Sundararajan , N. , 1996...

.... The effectiveness of the overall active control framework—an active compressor stability management system—is assessed using a computer simulation of a high-bypass, dual-spool, commercial-type turbofan engine. 25 03 2009 09 04 2009 04 03 2010 04 03 2010 aerospace engines aircraft...

... 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...