AvionicsData: Bus Avioniques Haut Débit et Réseaux Déterministes AFDX
AvionicsData fournit les spécifications de réseaux et commutateurs pour bus aérospatiaux, acheminant commandes de vol, flux radar et écrans cockpit sur des réseaux ARINC 664 (AFDX) et TTEthernet tolérants aux pannes.
AvionicsData Deterministic ARINC 664 / TTEthernet Avionics Bus Architecture
Virtual link traffic policing, dual-redundant fiber switches, and sub-microsecond PTP clock sync
Central System: AFDX Core Switch - Virtual Link Traffic Regulator
Aviation Architecture Nodes
- Flight Control Computer LRU
- Deterministic AFDX Fiber Switch
- Time-Triggered Ethernet (TTE) Hub
- High-Definition Cockpit Display Node
- Crash-Survivable Optical Data Sink
Architectural Layers & Protocol Stacks
- Deterministic Physical Layer & Optical Fiber (1000BASE-T1 / ARINC 818 High-Speed Video Fiber): Routing gigabit-rate sensor and radar streams with complete immunity to lightning strikes and electromagnetic interference (EMI).
- Time-Triggered Media Access & Synchronization (SAE AS6802 TTEthernet / IEEE 802.1AS PTP): Synchronizing all onboard computers to a fault-tolerant global clock with jitter under 1 microsecond.
- Virtual Link Policing & Traffic Isolation (Bandwidth Allocation Gap (BAG) Hardware Shapers): Preventing babbling-idiot faults by strictly policing transmission intervals and allocating dedicated bandwidth per Virtual Link.
- Integrated Modular Avionics (IMA) Transport (ARINC 653 Sampling & Queuing Ports): Interfacing RTOS software partitions directly with network frames without CPU interrupt thrashing.
Flight Telemetry Metrics: < 1 µs (Global Clock Synchronization Jitter) | Zero Loss (Virtual Link Packet Drop Guarantee) | 10 Gbps (High-Speed Fiber Avionics Bandwidth) | DO-254 DAL A (Hardware Switch Silicon Level)
Bus de données avioniques haut débit, ARINC 664 (AFDX), Ethernet déclenché par le temps et télémétrie de vol
Authoritative technical engineering reference for high-bandwidth avionics data buses, arinc 664 (afdx), time-triggered ethernet & flight telemetry in FAA Part 135/27, DO-178C DAL A avionics software, DO-254 hardware, 4D trajectory deconfliction, and ASTM F3411 Remote ID.
Core Engineering Areas
Technical Publications
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