Aerospace Instrument-Making Annotation << Back FEDERATIVE-INTEGRATED DISTRIBUTED MODULAR AVIONIC V.S. Kulabukhov The evolution of aircraft avionics suit digital computing system architectures is analyzed and the heuristicity of their synthesis approaches is shown. On the science based teleocentric approach the conception of a federative-integrated distributed (networked) modular avionics («FIRMA») is formulated and the routine, formalized procedure for analyze (decomposition) and synthesis (optimization) of topology of airborne distributed computing systems for avionics suites, integrated flight control systems and avionics in the whole is offered. Key words: avionics, structure, architecture, distributed computing system (network), avionics suit, flight control system. Contacts: E-mail: nit@mnpk.ru; kws0704@mail.ru Pp. 11-31.