AvionicsNodes: Aviônica Modular Integrada e LRUs de Borda ARINC 653

O AvionicsNodes estabelece especificações de arquitetura aberta para Aviônica Modular Integrada (IMA), empacotando processamento multicore de alta densidade, silício DO-254 DAL A e particionamento robusto ARINC 653 em LRUs robustecidas e resfriadas por convecção.

AvionicsNodes Integrated Modular Avionics (IMA) Node Architecture

Multicore processor, ARINC 653 robust partitioning, and ruggedized VPX backplane

Central System: IMA Processing Core - Multicore DO-254 / ARINC 653 Node

Aviation Architecture Nodes

  • Multicore Lockstep CPU
  • ARINC 653 Time/Space Enclave
  • Ruggedized OpenVPX Backplane
  • Discrete & Serial I/O Module
  • Aircraft Health Maintenance Unit

Architectural Layers & Protocol Stacks

  • Ruggedized Physical & Thermal Enclosure (Conduction-Cooled ATR Chassis / VITA 48 REDI): Dissipating 200W of heat without external fan air, surviving 20g shock and sustained aerospace vibration.
  • Silicon Hardware Safety Enclave (DO-254 DAL A FPGA / Fault-Tolerant Multicore): Providing lockstep execution, ECC memory scrubbing, and hardware watchdog timers to catch single-event upsets.
  • Spatial & Temporal Memory Partitioning (ARINC 653 Operating System Hypervisor): Guaranteeing that a software fault in a low-criticality app cannot starve CPU time or corrupt flight-critical memory.
  • Open System Architecture Interoperability (FACE Technical Standard / SOSA Consortium): Enabling rapid plug-and-play swapping of flight software modules across diverse airframe platforms.

Flight Telemetry Metrics: DO-254 DAL A (Hardware Silicon Certification Level) | -55°C to +105°C (Operational Temperature Range) | Zero Crosstalk (ARINC 653 Spatial Partitioning) | VITA 48 REDI (Ruggedized Conduction-Cooled Standard)

Aviônica Modular Integrada (IMA), Unidades Substituíveis em Linha (LRUs) e Computação de Borda ARINC 653

Referência técnica autoritativa para integrated modular avionics (ima), line replaceable units (lrus) & arinc 653 edge compute em certificações FAA Parte 135/27, software de aviônica DO-178C DAL A, hardware DO-254, desconflito de trajetórias 4D e Remote ID ASTM F3411.

Core Engineering Areas

Technical Publications

Related Cluster Architecture Specifications