Documento:
The FG105-A01 is a reliable, cost-effective fiber optic gyro strapdown inertial navigation system designed for UAVs, unmanned vehicles, ships, and aircraft navigation, control, and survey missions.
Featuring modular design, it integrates high-precision fiber optic gyros and FM accelerometers. The system fuses INS and GPS data via advanced filtering algorithms to estimate and compensate inertial errors, delivering accurate attitude, velocity, and position outputs. Custom vehicle motion constraints are available for land platforms to sustain long-term precise positioning.
Supporting flexible software function configurations including transfer alignment, integrated navigation, pure inertial calculation, and attitude-heading reference, this system can be customized to meet various industrial application demands.
| Fiber Optic Gyroscope | |
|---|---|
| Range (°/s) | ±500 |
| Bias (°/h) | ≤1 |
| Bias Stability (°/h, 10s) | ≤0.5 |
| Bias Instability (°/h, allan, typ) | ≤0.05 |
| Bias Repeatability (°/h, 6 power cycles) | ≤0.5 |
| Angle Random Walk (°/√h) | ≤0.05 |
| Scale Factor Nonlinearity (ppm) | ≤200 |
| Cross-Coupling (rad) | ≤0.001 |
| Bandwidth (Hz) | ≥200 |
| FM Accelerometer | |
| Range (g) | ±30 |
| Full-Temperature Bias (mg, 3σ) | ≤0.5 |
| Bias Stability (μg, 10s smoothing) | ≤10 |
| Bias Instability (μg, allan, typ) | ≤3 |
| Bias Repeatability (μg) | ≤10 |
| Velocity Random Walk (m/s/√h) | ≤0.01 |
| Scale Factor Nonlinearity (ppm, ±1g) | ≤100 |
| Cross-Coupling (rad) | ≤0.001 |
| Bandwidth (Hz) | ≥200 |
| Integrated Navigation Accuracy | |
| Integrated Heading Accuracy (°, 1σ, Real-time) | 0.5 |
| Integrated Horizontal Attitude (°, 1σ, Real-time) | 0.06 |
| Integrated Heading Accuracy (°, post-processing) | 0.06 |
| Integrated Horizontal Attitude (°, post-processing) | 0.01 |
| Integrated Horizontal Position (m, 1σ) | 3 (single point), 0.02+1ppm (RTK) |
| Integrated Vertical Position (m, 1σ) | 5 (single point), 0.03+1ppm (RTK) |
| Integrated Horizontal Velocity (m/s, 1σ) | 0.1 |
| Integrated Vertical Velocity (m/s, 1σ) | 0.15 |
| GNSS Receiver (External) | |
| Timing Accuracy | 20 ns |
| Cold Start Positioning Time | ≤40 s |
| Startup Time | ≤2s |
| Positioning Data Update Rate | 10Hz |
| Operating Altitude | 10,000 m |
| Satellite Mode | GPS: L1/L2/L5; BeiDou: B1/B2/B3; GLONASS: L1/L2 |
| Electrical/Mechanical Interface | |
| Power (V) | 12~36VDC (recommended 24V) |
| Steady-state Power (W) | ≤10W |
| Startup Time (s) | 3 |
| Communication Interface | RS-422 |
| Update Rate (Hz, max) | 1000 (IMU), 200 (INS) |
| Dimensions (mm*mm*mm) | 65*70*63 |
| Weight (g) | ≤500 |
| Operating Environment | |
| Operating Temperature | -40°C to +70°C |
| Storage Temperature | -55°C to +85°C |
| Vibration | 20~2000Hz, 6.06g |
| Shock | 100g/1ms |
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