NTNNavigation | 无人系统天基自主导航、紧耦合惯导融合与轨道伪卫星增强系统

NTNNavigation 为自主机器人、无人机与无人货船设计高韧性导航方案,将星载 5G 信号与高精度惯导 (IMU) 及在轨伪卫星深度耦合。

NTNNavigation Deep Inertial Space-Coupled Architecture

Tight Kalman integration of satellite pseudorange vectors with tactical MEMS gyros

Central System: Tactical-Grade MEMS IMU - Fiber-optic gyro grade drift (<0.1 deg/hr)

Network Nodes

  • Tactical-Grade MEMS IMU
  • LEO Satellite Pseudolite Receiver
  • Tightly-Coupled Extended Kalman Filter
  • Autonomous Flight / Autopilot

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)

自主系统空间导航、深组合惯性导航 (INS) 与星载伪卫星 (Pseudolite)

Core Engineering Areas

Technical Articles

Related Cluster Architecture Specifications