Abstract
Typical avionics system integration architecture describes representatives of typical engineering integrated technical architecture in the development history of avionics systems. Through the balance between technological advancement and technological effectiveness, the balance between system organization and system complexity, and the balance between application requirements and development costs, the typical representatives of avionics system integration technology architecture are formed: the federated system architecture, integrated modular avionics (IMA) system architecture, and distributed integrated modular avionics (DIMA) system architecture.
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