32th Congress of the International Council of the Aeronautical Sciences

02 - Systems Engineering and Integration

MODEL-BASED VIRTUAL INTEGRATED TEST METHOD FOR AVIONICS SYSTEM

S.F. Zhu╣, P.P. Xing╣; ╣COMAC Beijing Aircraft Technology Research Institute, China

This paper proposes a model-based virtual integrated test method for avionics systems. This method realizes multi-model integration, full-life cycle model delivery and two-way traceability with top-level requirements, and solves the problems of low test efficiency and poor feasibility of complex interface cross-linking tests in the early verification of avionics systems.


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