optic integrated navigation system INS with closed-loop fiber optic gyroscopes, accelerometers, and high-end GNSS
The fiber optic integrated navigation system GA300 is based on cost-effective closed-loop fiber optic gyroscopes, accelerometers, and high-end GNSS receiving boards. It is implemented through multi-sensor fusion and navigation solution algorithms to meet the requirements of high-precision mobile measurement systems, large UAVs and other applications The field requires precise measurement of information such as attitude, heading and position.
Parameters | Index | |
Position accuracy | Single point (RMS) | 1.2m |
RTK(RMS) | 2cm+1ppm | |
Post-processing (RMS) | 1cm+1ppm | |
Loss lock accuracy (CEP) | 3nm(30min)10nm(1h) | |
Heading (RMS) | Single antenna | 0.05°③ |
0.02°(Post-processing) | ||
Dual antenna | 0.1°(Baseline≥2m) | |
Loss lock retention accuracy | 0.25°(Loss lock 30min)0.5°(Loss lock 1h) | |
North seeking accuracy | 1°SecL, alignment 15min | |
Attitude (RMS) | Single antenna | 0.02° |
Dual antenna | 0.02° | |
Post-processing | 0.01° | |
Loss lock retention accuracy | 0.25°(Loss lock 30min)0.5°(Loss lock 1h) | |
Horizontal speed accuracy (RMS) | 0.05m/s | |
Output frequency | 200Hz | |
Gyro | Range | 400°/s |
Zero bias stability | 0.2°/h⑤; | |
Scaling factorNon-linearity | 100ppm | |
Angle random walk | 0.05°/√hr | |
Accelerometer | Range | 16g |
Zero bias stability | 50ug⑤ | |
Scaling factorNon-linearity | 100ppm | |
Speed random walk | 0.01m/s/√hr | |
Dimensions and electrical characteristics | Size | 139 mm×136.5 mm×101mm |
Weight | <2.7kg (not include cable) | |
Input voltage | 12~36VDC | |
Power consumption | <24W (Steady state) | |
Environmental indicators | Working temp. | -40℃~+60℃ |
Random vibration | 6.06g,20Hz~2000Hz | |
MTBF | 30000h | |
Interface | PPS,EVENT,RS232,RS422,CAN (optional) | |
Antenna interface | ||
Wheel speed sensor interface |