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| Categories | Fiber Optic Gyro | 
|---|---|
| Brand Name: | Firepower | 
| Model Number: | FOG-50-MP | 
| 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 | 
| Zero bias stability: | ≤0.2°/h | 
| Random walk coefficient: | ≤0.03°/√h | 
| Measuring range: | -500~+500°/s | 
| Start time: | 3s | 
| Impact: | 30g, 11ms | 
| Vibration: | 20~2000Hz, 0.06g²/Hz | 
| Output mode: | RS422 | 
| Working temperature: | -40~+70℃ | 
| Storage temperature: | -55~+85℃ | 
| Power consumption: | ≤6W | 
| Company Info. | 
| Shenzhen Fire Power Control Technology Co., LTD | 
| Verified Supplier | 
| View Contact Details | 
| Product List | 
1. Principle of operation
The implementation of fiber optic gyroscopes is mainly based on the
Sagnac theory: the Sagnac effect describes the interference
phenomenon of light in a rotating reference system: when light
propagates in a closed loop (e.g., a fiber optic ring) in the
clockwise and counterclockwise directions, if the system is in a
rotating state, the optical paths of the two beams of light show a
small time difference, leading to a phase difference. This phase
difference is proportional to the rotational angular velocity and
can therefore be used to measure rotational motion. This is how
fiber optic gyroscopes work.
2. Parameters
| Serial number | Test item | Unit | Technical requirements | 
| 1 | Overall dimensions | mm | 50×50×32 | 
| 2 | Start-up time | s | 3 | 
| 3 | Zero bias | (°)/h | ≤1 | 
| 4 | Zero bias stability at normal temperature (constant temperature) (10 s smooth) | (°)/h | ≤0.2 | 
| 5 | Zero bias stability with temperature change (1 ℃/min variable temperature, 100 s smooth) | (°)/h | ≤0.5 | 
| 6 | Zero-bias repeatability | (°)/h | ≤0.1 | 
| 7 | Zero bias sensitivity | (°)/h/Gs | ≤0.5 | 
| 8 | Random walk coefficient | (º)/h1/2 | ≤0.03 | 
| 9 | Scale factor nonlinearity | ppm | ≤20 | 
| 10 | Scale factor asymmetry | ppm | ≤5 | 
| 11 | Scale factor repeatability | ppm | ≤10 | 
| 12 | Threshold | (°)/h | ≤0.2 | 
| 13 | Resolution | (°)/h | ≤0.2 | 
| 14 | Bandwidth | Hz | ≥500 | 
| 15 | Operating temperature | ℃ | -45~+70 | 
| 16 | Storage temperature | ℃ | -55~+85 | 
| 17 | Dynamic range | (°)/s | ±500 | 
| 18 | Supply voltage | V | +5 | 
| 19 | Normal temperature steady state power consumption | W | ≤2.5 | 
| 20 | Full temperature steady state power consumption | W | ≤4 | 
| 21 | Start the instantaneous current | A | <1.5 | 
3. Characteristics compared to other types of gyroscopes
| Gyro Type | Key Benefits | Major Disadvantages | 
| Fiber optic gyroscope(FOG) | High precision, no mechanical parts, anti-interference | Higher price | 
| Ring laser gyroscope(RLG) | High accuracy for aerospace | Large size and high cost | 
| Mechanical gyroscope(MG) | Traditional and reliable for low-end applications | Mechanical components are prone to wear and tear, high maintenance costs | 
| MEMS gyro | Small size and low cost | Lower accuracy, susceptible to environmental factors | 
4. High Accuracy and Stability
The fiber optic gyroscope adopts the advanced Sagnac effect
detection technology, which provides high angular velocity
measurement accuracy (up to 1°/h or less) and excellent zero-bias
stability over long periods of time, ensuring that reliable
navigation and attitude control data can still be provided in
complex environments.
5. Production environments
|   | 
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