Volume 25 Issue 9
Sep.  2010
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YAO Hua-ting, WANG Xi, SU San-mai. Integrative simulation platform design for aero-engine digital electronic control system[J]. Journal of Aerospace Power, 2010, 25(9): 2148-2154.
Citation: YAO Hua-ting, WANG Xi, SU San-mai. Integrative simulation platform design for aero-engine digital electronic control system[J]. Journal of Aerospace Power, 2010, 25(9): 2148-2154.

Integrative simulation platform design for aero-engine digital electronic control system

  • Received Date: 2009-08-18
  • Rev Recd Date: 2009-03-13
  • Publish Date: 2010-09-28
  • Combined with existing software and hardware resources,integrative simulation platform for aero-engine digital electronic control system,which mainly includes aeroengine model subsystem,signal simulation and processing subsystem,controller rapid prototyping subsystem was designed with modular approach.Aero-engine model subsystem acts as a numerical simulation platform that calls aero-engine mathematical model library and mechanical hydraulic actuator mathematical model library.Rapid prototyping subsystem for controller runs in Matlab/Simulink environment,in which control code encapsulated into S-Function module.As key techniques in platform software design,mixed programming and WINDOWS timer programming method were described in detail.Applying the platform to a turbofan control system researchment,numerical simulation,semi-physical simulation and bed test results are consistent.It shows the platform is feasible and effective in engineering.

     

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