Abstract
The control system of aeroengine design is a complex system engineeringincludingmany procedure of different subsystems. To improve the efficiency of areoengine control system design and reduce the cost and development period of research procedure, model-based areoengine control system design method can be used for integrating systems, collaborative design and optimizing design. Model-based aeroengine control system design workflow consists of the phases from analysis of system requirements to semi-physics simulation verification. The management approach and design procedure can help to separate the whole design workflow into different sub-phases which can help to scheme the concurrent design procedure of complex control system in order to improve the
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