AvionicsDigitalTwins: Co-Simulação Hardware-Software e Sombras Digitais em Voo

O AvionicsDigitalTwins cria réplicas digitais precisas ao nível de ciclo de suítes aviônicas completas, combinando emulação virtual QEMU, simulação de barramentos ARINC 664 e sombreamento de telemetria em tempo real para detectar anomalias e ameaças cibernéticas em voo.

AvionicsDigitalTwins Synchronized In-Flight Digital Shadow Architecture

Cycle-accurate CPU emulation, virtual data bus fabric, and discrepancy anomaly detector

Central System: Virtual Avionics Host - Cycle-Accurate Co-Simulation Core

Aviation Architecture Nodes

  • Physical Aircraft Avionics Suite
  • Air-to-Ground Telemetry Diode
  • Cycle-Accurate Virtual LRU Cluster
  • Virtual ARINC 664 Bus Fabric
  • Discrepancy & Cyber Intrusion Detector

Architectural Layers & Protocol Stacks

  • Instruction Set Emulation & Virtualization (QEMU Aerospace Fork / SystemC TLM-2.0): Executing unmodified aircraft binary firmware with cycle-accurate register and memory timing.
  • Virtual Network & Bus Interconnect (Simulated AFDX / Virtual ARINC 429 Transceivers): Routing simulated packets between virtual LRUs with exact microsecond transmission delays and jitter.
  • Parallel Digital Shadowing & Comparison (State Machine Discrepancy Comparator): Comparing physical aircraft telemetry with virtual twin outputs, flagging unintended software drift or cyber tampering.
  • Post-Flight Debugging & Root-Cause Analysis (Deterministic Execution Replay / Time-Travel Debug): Allowing software engineers to step backward in time through CPU execution to pinpoint intermittent flight glitches.

Flight Telemetry Metrics: 100% (Binary Code Execution Parity) | < 1 Frame (Digital Shadow State Divergence Lag) | Time-Travel (Deterministic Microsecond Replay) | Zero Hardware (Requirement for Virtual Test Clusters)

Gêmeos de Co-Simulação Hardware-Software de Aviônica, Injeção de Falhas e Detecção de Anomalias em Voo

Referência técnica autoritativa para avionics hardware-software co-simulation twins, fault injection & in-flight anomaly detection 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