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| Categories | Fiber Optic Gyro | 
|---|---|
| Brand Name: | Firepower | 
| Model Number: | 3OG-120H | 
| Certification: | CE | 
| Place of Origin: | China | 
| MOQ: | 1 | 
| Price: | Negotiable | 
| Payment Terms: | T/T | 
| Supply Ability: | 500/month | 
| Delivery Time: | 10 days | 
| Packaging Details: | sponge and carton | 
| Measuring range: | -500~+500°/s | 
| Zero bias stability: | ≤0.005°/h (10s smoothing) | 
| Random walk coefficient: | ≤0.0005°/√h | 
| Zero bias repeatability: | ≤0.0015°/h | 
| Scale factor asymmetry: | ≤2ppm | 
| Threshold: | ≤0.002°/h | 
| Dimensions: | 60±0.1×60±0.1×28.0±0.1(L×W×H; mm) | 
| Weight: | ≤2300g | 
| Company Info. | 
| Shenzhen Fire Power Control Technology Co., LTD | 
| Verified Supplier | 
| View Contact Details | 
| Product List | 
1. Product Overview
The 3-axis integrated Fiber Optic Gyroscope (FOG, Fiber Optic
Gyroscope) is a high precision angular velocity sensor based on the
principle of optical interference. It detects angular velocity by
measuring the Sagnac effect generated when light propagates along
the fiber optic ring and outputs precise attitude information.
Compared to traditional mechanical gyroscopes, the FOG has the
advantages of being frictionless, long-life, high-precision and
shock-resistant, making it a core component in modern inertial
navigation and attitude measurement systems.
The integrated three-axis design means that the gyroscope can
measure the angular velocity in X, Y, and Z directions
simultaneously, simplifying system integration and improving
attitude measurement accuracy, which is widely used in aerospace,
navigation, robotics, precision measurement, and other fields.
2. Main Product Features
A. High precision: Compared with MEMS gyroscope, FOG has lower
offset drift and higher angular velocity resolution, which is
suitable for high-precision navigation systems.
B. Three-axis integration: No need to combine multiple gyros,
reducing volume and weight, improving system integration and
reliability.
C. No mechanical moving parts: Compared to mechanical gyroscopes,
FOG is frictionless and wear-free, resulting in longer life and
higher reliability.
D. Resistant to vibration and shock: Suitable for highly dynamic
environments such as drones, missiles, and flying machines.
Ready-to-use, no warm-up required: Compared to laser gyroscopes
(RLG), FOG has a short start-up time and fast response.
E. Low-power design: Optimized energy consumption for
battery-powered systems such as UAVs and portable navigation
devices.
3. Parameters
| Serial number | Test item | Unit | Technical requirements | 
| 1 | Start-up time | min | Power-on bias stability index | 
| 2 | Zero bias stability at room temperature (constant temperature) | (°)/h | ≤ 0.005 (10 s smoothing) ≤ 0.0015 (100 s smoothing) | 
| 3 | Zero bias stability with temperature change (1 ℃/min variable temperature, 100 s average) | (°)/h | ≤0.01 | 
| 4 | Zero-bias repeatability | (°)/h | ≤0.0015 | 
| 5 | Random walk coefficient | (º)/h1/2 | ≤0.0005 | 
| 6 | Scale factor nonlinearity | ppm | ≤5 | 
| 7 | Scale factor asymmetry | ppm | ≤2 | 
| 8 | Scale factor repeatability | ppm | ≤10 | 
| 9 | Scale factor repeatability (full temperature) | ppm | ≤50 | 
| 10 | Operating temperature | ℃ | -40~+60 | 
| 11 | Storage temperature | ℃ | -50~+70 | 
| 12 | Dynamic range | (°)/s | ±500 | 
| 13 | Supply voltage | V | +5V | 
| 14 | Steady-state power consumption | W | < 4 (normal temperature) < 8 (full temperature) | 
|   | 
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