AvionicsData: Buses de Aviónica de Gran Ancho de Banda y Redes Deterministas AFDX
AvionicsData proporciona especificaciones de ingeniería de redes y switches para buses aeroespaciales, encaminando control de vuelo, sensores radar y pantallas de cabina mediante redes tolerantes a fallos ARINC 664 (AFDX) y TTEthernet.
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)
Buses de Datos Aviónicos de Alto Ancho de Banda, ARINC 664 (AFDX), Ethernet Activado por Tiempo y Telemetría de Vuelo
Referencia técnica autorizada para high-bandwidth avionics data buses, arinc 664 (afdx), time-triggered ethernet & flight telemetry en regulaciones FAA, software de aviónica DO-178C DAL A, hardware DO-254 e integración UTM.
Core Engineering Areas
Technical Publications
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