Aircraft engine part modeling method based on control system development platform
An aero-engine and development platform technology, applied in general control systems, control/regulation systems, simulators, etc., can solve problems such as low interaction efficiency and large modeling workload, avoiding repeated modeling processes and simplifying interaction methods. , the effect of improving the efficiency of interaction between departments
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[0019] This embodiment is an aeroengine component modeling method based on a control system development platform.
[0020] Refer to Figure 1 ~ Figure 4 , Based on the aero engine component modeling method of the control system development platform, based on the Pascal language source code of GasTurb, add the necessary code, in Del x Build dynamic link library A with extension DLL under hi platform. The dynamic link library B with the extension name of MEXW32 is established in MATLAB with the S function interface technology of C / C++ mode. Through the call of dynamic link library B to dynamic link library A and engine model configuration files, the engine component-level dynamic model of GasTurb can be directly called in MATLAB / Simulink in a graphical module. Among them, the dynamic link library A contains the gasturb engine component-level dynamic model calculation function, but does not contain the model parameters; the dynamic link library B contains the main calculation progr...
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