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To improve the control performance in the transient state of a gas turbine engine, a new method based on variable replacement method (VRM) and particle swarm optimization (PSO) algorithm is proposed. Above all, an acceleration schedule under the constraints of fuel air ratio ($FAR$ ), high pressure turbine inlet temperature ($T_{4}$ ) and high pressure compressor surge margin ($SM$ ) could be obtained...
A novel control scheme for a thrust vector system with an electromechanical actuator is proposed. The proposed method merges the idea exploited in sliding mode control (SMC) with proportion–integration–differentiation (PID) control, which brings advantages in terms of strong robustness and good position tracking performance, while the chattering of the control signal produced by the SMC is small....
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