◆ Features
I-FOG-10 is all-solid and has good anti-vibration performance. It adopts photoelectric integrated and all-digital closed-loop control design; At the same time, it has excellent anti-magnetic field performance, temperature resistance, and environmental adaptability.
◆Applications
The product is suitable for airborne navigation, payload attitude determination, and positioning and orientation systems. It can be widely used in military fields such as unmanned aircraft, warships, land positioning/orientation, and in civil fields such as ships, general aviation, and track inspection.
◆ Specifications
P/N | I-FOG-10-01 | I-FOG-10-02 | Note |
Bias Stability | ≤0.005°/h | ≤0.005°/h | 1σ, 100s smooth |
Bias Stability in Full Temperature | ≤0.01°/h | ≤0.02°/h | 1σ, 100s smooth |
Scale Factor Nonlinearity | ≤10ppm | ≤10ppm | |
Scale Factor Asymmetry | ≤10ppm | ≤10ppm | |
Measuring Range | ±300°/s | ±300°/s | |
Random Walk Coefficient | 0.001°/√h | 0.001°/√h | |
Frequency Bandwidth | ≥150Hz | ≥150Hz | |
Weight | ≤480g | ≤480g | |
Maximum Power Consumption | ≤5W | ≤5W | |
Working Temperature | -40°C~65°C | -40°C~65°C | |
Output Mode | RS422 | RS422 | Can be customized according to user requirements |
Power Supply | ±5V±0.15V | ±5V±0.15V | |
Size | 98x98x35mm | 98x98x35mm | Interface pin not included |