Abstract
The simulation of an aero-engine control system involves numerous disciplines due to its complex functions and architecture, which generally consist of mechanical, hydraulic and electrical, and electronic systems. For each discipline, the modeling and simulation are usually dependent on different commercial software and tools, which makes the simulation, integration, and verification of system-level models very difficult. To meet this challenge, a multi-domain co-simulation method based on the Functional Mock-up Interface (FMI) standard is proposed to integrate models developed by different software or tools. The simulation and testing results demonstrate that multi-disciplinary model integration and cross-platform simulation based on the FMI standard can be realized for an aero-engine control system, which lays a foundation for high-fidelity control system design, simulation, integration, and testing.
Funder
Fundamental Research Funds for the Central Universities
Central Military Commission Foundation to Strengthen Program Technology Fund
Reference28 articles.
1. Research of Model-based Aeroengine Control System Design Structure and Workflow
2. Numerical Propulsion System Simulation (NPSS) 1999 Industry Review;Lytle,2000
3. Summary of CORBA Technique;Wang;Comput. Sci.,1999
4. Summary of HLA and the key technologies in simulation applications;Xu;Comput. Simul.,2001
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