NTNNavigation | 자율 시스템 우주 항법, 관성 센서 융합 및 궤도형 의사위성 증강 시스템

NTNNavigation은 자율 로봇, 드론 및 자율 선박을 위한 복원력 있는 항법을 설계하여 위성 5G 신호와 고성능 관성 측정 장치(IMU) 및 우주 의사위성을 융합합니다.

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)

자율 시스템 우주 항법, 심층 관성 통합 및 우주 의사위성(Pseudolite)

Core Engineering Areas

Technical Articles

Related Cluster Architecture Specifications