Product Introduction
GSINS016C series inertial navigation system is a typical shelf product. With high-performance fiber optic gyro and accelerometer,GSINS016C series inertial navigation can meet the needs of autonomous navigation in complex environments, and can integrate satellite, Doppler, odometer and other information to achieve high-precision integrated navigation. Series products have been widely used in military defense, maritime, aerospace, automatic control, mapping and other fields.
GSINS016C is a medium-precision fiber-strapdown inertial navigation system with a heading alignment accuracy better than 0.1° (1σ) and a pure inertial navigation accuracy better than 2nm/h (CEP).
Technical Specifications
| Parameter | GSINS016C | |||
| Power dissipation | ≤20W | |||
| Dimension | 110×110×100mm | |||
| Weight | 1.6kg | |||
| Input voltage | 18V~36V | |||
| Service temperature | -40℃~+60℃ | |||
| Mechanical environment | strike | Half sine wave 20g, 11ms | ||
| Vibration | GJB150.16A-2009 | |||
| MTBF | ≥30000h | |||
| External interface | RS422; CAN; Network port; Odometer interface |
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| System Performance | ||||
| GSINS008C | ||||
| Location | Pure inertia | ≤2nm/10min,CEP | ||
| Satellite combination | ≤5m,CEP | |||
| DVL combination | ≤1%D,CEP | |||
| Course | ≤1.0°,1σ | |||
| Posture | ≤0.2°,1σ | |||
| Alignment time | 5min | |||
| Device Performance | ||||
| GSINS008C | ||||
| Peg-top | Zero bias stability | ≤0.1°/h,1σ | ||
| Zero bias repeatability | ≤0.1°/h,1σ | |||
| Scale factor | ≤100ppm,1σ | |||
| Random walk | ≤0.01 °/ √h | |||
| Accelerometer | Zero bias repeatability | ≤100ug,1σ | ||
| Zero bias stability | ≤100ug,1σ | |||
| Scale factor repeatability | ≤100ug,1σ | |||
| Scale factor stability | ≤100ug,1σ | |||
Application