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Aerospace RLG INS(Dubhe-A20)
Designed for modern airborne platforms, this optical INS features FOG/RLG technology with quartz accelerometers in optimized strapdown architecture. The system's fusion engine integrates GNSS, celestial, and other navigation data while maintaining pure inertial capability.
Perfect for UAV operations
its highlights include:
1) Vibration-resistant alignment;
2) Flexible alignment options;
3) Expandable sensor integration;
4) Built-in system diagnostics.
Series | Aerospace Inertial Navigation System(INS-A) | ||
Type | Dubhe-A20 | ||
Accelerometer | Months Bias Repeatability(1σ) | ≤10μg | |
Months Scale Factor Accuracy(1σ) | ≤10ppm | ||
Gyro | Bias Repeatability(1σ) | ≤0.008°/hr | |
Scale Factor Accuracy(1σ) | ≤10ppm | ||
Random walk(1σ) | ≤0.003°/√hr | ||
Features | Position Accuracy | Pure inertia | ≤1nm/20h,CEP |
INS/GNSS combination | better than GNSS | ||
Speed Accuracy | Pure inertia | ≤1.0 m/s,RMS | |
INS/GNSS combination | ≤0.2m/s,RMS | ||
Angular Rate | ≥±400°/sec | ||
Angular Acceleration | 100000°/sec2 | ||
Acceleration | >25g | ||
Angular Attitude | Any Orientation | ||
Alignment time | ≤30min | ||
Input/output | 3 RS422 full-duplex serial ports, 1 100M Ethernet port | ||
Alignment time | Time | <30min | |
AHRS Applications Performance | Heading Accuracy | Pure inertia | ≤0.02°sec(L),RMS |
INS/GNSS combination | ≤0.01°,RMS | ||
Pitch & Roll Accuracy | Pure inertia | ≤0.015°,RMS | |
INS/GNSS combination | ≤0.01°,RMS | ||
Characteristics | Power consumption | <40W | |
Dimensions | 232×186×160 | ||
Weight | <8.2kg | ||
Temperature | -40℃~60℃ | ||
Shock | 15g,Half-sine wave 11ms | ||
Input Voltage | DC24V(±25%) | ||
cooling | Conduction to mounting plate | ||
Vibration | 20~2000Hz,6.06g | ||
MTBF | >10000 hours |