AerospaceDigitalTwins: 物理引导航天数字孪生与实时结构应力遥测系统

AerospaceDigitalTwins 将多物理场有限元/计算流体力学与真实轨道遥测数据流深度耦合,实现前瞻性飞行器结构健康监测与包线仿真。

AerospaceDigitalTwins High-Fidelity In-Flight Synchronization Mesh

Coupled boundary element modeling, kalman filtering, and edge state estimation

Central System: Fiber Bragg Grating Array - Distributed optical strain and temperature sensing

Network Nodes

  • Fiber Bragg Grating Array
  • Onboard State Estimator
  • Distributed High-Performance Twin
  • Remaining Useful Life (RUL) Core

Architectural Protocol Layers

  • Spaceborne PHY/MAC Layer (3GPP Rel-17 TS 38.300): Doppler compensation, HARQ disabling, and timing advance extension.
  • Orbital Mesh Routing (CCSDS / Delay-Tolerant Networking): Dynamic topology routing over intermittent laser crosslinks.
  • Regenerative Core Processing (OpenRAN / 3GPP CU-DU Split): Onboard user plane function (UPF) local breakout.

Key Metrics: < 18ms (LEO Orbit-to-Ground Roundtrip) | 100 Gbps (Optical Crosslink Throughput) | ±48 kHz (Doppler Shift Compensation) | 99.999% (Orbital Constellation Availability)

融合物理规律的航空航天数字孪生体、在轨实时遥测镜像与全生命周期预测分析

Core Engineering Areas

Technical Articles

Related Cluster Architecture Specifications