Expandable Optimum Avionics Architecture Solution with Advantage in terms of Cabling Weight for a Helicopter

One of the biggest problems that aviation industry focuses on in helicopter platforms is payload not at desired level. Another these integration problem experienced process integrating current technological equipment into avionics architecture later throughout product life cycle helicopter. Increasing allows to carry more personnel, ammunition, etc. An expandable concept enables this if it integrate new In context, R&D activities are organized order for be fast, and reliable, transfer data via lighter ways. study, avionic architectural concepts from past present were examined a comparative analysis was made terms cabling weight will formed platform its possible use. While creating concept, distributed, federated, integrated distributed architectures examined, as well RS-422/485, ARINC-429/629, AFDX, MIL-STD-1553 FIBRE Channel protocols within scope communication protocols. By examining superiority mentioned each other, created by different calculated, optimum which could expanded create minimum military type helicopter, proposed.