SD701 MEMS Integrated Inertial Navigation System
Applications
Suitable for the field of attitude measurement and navigation of drones.
Main Technical Specifications
Parameter | Technical specification | |
System Specifications | Position accuracy | < 10m (1σ) |
Heading accuracy (180s) | ≤2° | |
Horizontal attitude accuracy | ≤2° | |
Start Time | 2s | |
Fiber Optic Gyro Specifications | Zero bias stability (1σ, 100s) | 30°/h |
Scale factor repeatability (1σ) | 0.1% | |
Measuring range | ±400°/s | |
Accelerometer Specifications | Zero bias stability (1σ, 100s) | 2mg |
Scale factor repeatability (1σ) | 0.3% | |
Measuring range | ±18 g | |
Physical Specifications | volume | 96mm×96mm×50mm |
weight | ≤ 0.35kg | |
Maximum power consumption | ≤ 5W | |
Operating temperature | -40 ℃ ~ 65 ℃ | |
Electrical Interface | RS422 | |
Power supply requirements | 18 ~ 36 VDC |