Navigation-Grade Airborne Laser Gyro INS With 1 nm/h CEP For Long-Endurance Aircraft

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The Dubhe-A1 is an airborne inertial navigation system built around high-grade optical gyroscopes for fixed-wing and rotary-wing platforms. It delivers ≤1 nm/1

SKU: Dubhe-A1 Category:

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Product Overview

The Dubhe-A1 is an airborne inertial navigation system built around high-grade optical gyroscopes for fixed-wing and rotary-wing platforms. It delivers ≤1 nm/1 h CEP pure-inertial position accuracy and reaches better-than-satellite accuracy with GNSS fusion, keeping precision through jammed or denied GNSS environments. Alignment completes within 5 minutes in any orientation, and RS-422 plus Ethernet interfaces integrate cleanly with mission computers.

Key Features

  • Pure-inertial position accuracy of ≤1 nm/1 h CEP
  • Pure-inertial heading accuracy of ≤0.05°·sec(L) RMS and ≤0.01° RMS RMS pitch/roll with INS/GNSS
  • Speed accuracy of ≤1.2 m/s RMS pure inertial and ≤0.2 m/s RMS with GNSS
  • Gyro bias repeatability ≤0.005°/hr and angular random walk ≤0.003°/√hr
  • Alignment time ≤5 min in any orientation; angular rate ≥±400°/s
  • Conduction-cooled 195×160×108 mm unit weighing ≤3.9 kg, MTBF ≥20,000 hours

Technical Specifications

Parameter Specification
Accelerometer bias repeatability (1σ, months) ≤30 μg
Accelerometer scale factor accuracy (1σ, months) ≤30 ppm
Gyro bias repeatability (1σ) ≤0.005°/hr
Gyro scale factor accuracy (1σ) ≤10 ppm
Gyro accuracy (10 s, 1σ) ≤0.01°/hr (100 s, 1σ)
Angular random walk (1σ) ≤0.003°/√hr
Position accuracy (pure inertial) ≤1 nm/1 h CEP
Position accuracy (INS/GNSS) Better than satellite accuracy
Speed accuracy (pure inertial) ≤1.2 m/s RMS
Speed accuracy (INS/GNSS) ≤ 0.2 m/s RMS
Angular rate ≥ ±400°/s
Angular acceleration 100,000°/s²
Acceleration ≥ 25 g
Attitude Any orientation
Alignment time ≤ 5 min
Interfaces 3 × RS-422 full-duplex, 1 × 100 M Ethernet
Heading accuracy (pure inertial) ≤0.05°·sec(L) RMS
Heading accuracy (INS/GNSS) ≤0.03° RMS
Pitch & roll accuracy (pure inertial) ≤0.03° RMS
Pitch & roll accuracy (INS/GNSS) ≤0.01° RMS
Power consumption ≤20 W
Dimensions (L×W×H) 195×160×108 mm
Weight ≤3.9 kg
Operating temperature -40℃ – +60℃
Shock 15 g half-sine, 11 ms
Supply voltage DC 24 V ±25%
Vibration 20–2000 Hz, 6.06 g
MTBF ≥ 20,000 hours

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