Turboshaft engine steady-state model identification method based on PSO-NARX
A PSO-NARX, turboshaft engine technology, applied in the field of engine modeling and regression identification, can solve the problems of complex accuracy, difficulty in establishing a steady state model of a turboshaft engine, etc., and achieves difficult and complex results.
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[0044] Embodiment 1, the PSO-NARX network proposed by the present invention is used for the identification process of the turboshaft steady-state model model as follows figure 1 shown.
[0045] The identification of the dynamic system requires a dynamic identification network architecture, using the input and output of the identified system as identification information, that is, using a serial-parallel structure to identify the engine starting process. The model identification architecture is as follows: figure 2 shown.
[0046] Aeroengine is a highly nonlinear time-varying system. Atmospheric static temperature T 0 , the absolute pressure altitude H p , flight Mach number Ma, and fuel flow G all affect the engine's working process and performance parameters. The main working state parameter of a turboshaft engine is the gas generator speed n g , engine exhaust temperature T 4 and engine torque T.
[0047] The current working state of the engine is closely related to ...
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