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| Categories | Fiber Optic Gyro |
|---|---|
| Brand Name: | Firepower |
| Model Number: | MFOG-910 |
| Place of Origin: | China |
| MOQ: | 1 |
| Price: | 700$ |
| Payment Terms: | L/C,D/A,D/P,T/T,Western Union |
| Supply Ability: | 500/month |
| Delivery Time: | 1 Week for sample |
| Packaging Details: | BOX+Sponge |
| Maximum Angular Rate: | ±240°/s |
| Bias Stability: | ≤0.8°/h |
| Zero Bias Repatability: | ≤0.8°/h |
| Random Walk Cefficient: | ≤0.02°/√h |
| Supply Voltage: | +5V |
| Output Type: | Analog |
| Band Width: | ≥1000Hz |
| Dimension: | 82mm × 82mm × 19.5mm |
| Company Info. |
| Shenzhen Fire Power Control Technology Co., LTD |
| Verified Supplier |
| View Contact Details |
| Product List |
Replacing the Fizoptika VG910, the MFOG-910 micro-nano fiber optic gyroscope delivers high reliability for aerospace and defense applications. Compact (82*82*19.5mm) and lightweight (≤150g), it features ±240°/s measurement range, scale factor 47±5 mV/°/s, zero-bias repeatability ≤0.8°/h, and 15-year life expectancy. The robust construction withstands random vibrations up to 20g and accelerations ≥70g, making it perfect for UAVs, tactical vehicles, and precision navigation platforms.
The product is mainly composed of the following components:
| Parameter | Performance Indicators |
|---|---|
| Range (°/s) | ±240 |
| Scale factor (mV/°/s) | 47±5 |
| Scale factor nonlinearity (ppm) | ≤1000 |
| Zero-bias stability (10s, 1σ, °/H) | ≤0.8 |
| Zero-bias repeatability (1σ, °/H) | ≤0.8 |
| 3dB Bandwidth (Hz) | ≥1000 |
| Random walk (°/√H) | ≤0.02 |
| Power supply (V) | 5±0.25±12 |
| Power Consumption (W) | ≤1.5 |
| Impact (g) | ≥1500 |
| Acceleration (g) | ≥70 |
| Life (years) | ≥15 |
| MTBF | ≥100000 |

The MFOG-910 fiber optic gyroscope is widely used in navigation, stabilization, and attitude measurement systems. Typical applications include:
The MFOG-910 is designed to provide equivalent or superior performance compared to the Fizoptika VG910 fiber optic gyroscope. Advantages include:
This makes the MFOG-910 an excellent choice for customers seeking a reliable replacement for Fizoptika VG910 in inertial navigation and stabilization applications.
| Parameter | VG910H1 Fiber Optic Gyroscope | MFOG-910 Micro-Nano Fiber Optic Gyroscope |
|---|---|---|
| Angular Rate Range (°/s) | 250 | ±240 |
| Bias Stability (RMS, °/h) | 1 | ≤0.8 |
| Angle Random Walk (°/√h) | 0.015 | ≤0.02 |
| Bandwidth (kHz) | 1 | ≥1 |
| Scale Factor Stability / Repeatability (RMS, %) | 0.02 | ≤0.1 |
| Start-up Time (s) | 0.03 | Fast start |
| Power Consumption (W) | 0.5 | ≤1.5 |
| Dimensions (mm) | 82 * 82 * 20 | 82 * 82 * 19.5 |
| Weight (g) | 150 | ≤150 |
| Operating Temperature (°C) | −40 ~ +70 | −40 ~ +70 |
| Storage Temperature (°C) | −55 ~ +85 | −55 ~ +85 |
| Vibration (RMS, 0.02-2 kHz, g) | 30 | 20 |
| Shock (g, 1 ms) | 1200 | ≥1500 |
| MTBF (20°C) | 100000 h | ≥100000 h |
| Lifetime | 15 years | ≥15 years |
A fiber optic gyroscope (FOG) is a high-precision angular rate sensor based on the Sagnac effect. It measures rotation by detecting the phase difference between two beams of light traveling in opposite directions inside a fiber coil. FOG sensors are widely used in inertial navigation systems, UAVs, robotics, and stabilization platforms.
Yes. The MFOG-910 micro-nano fiber optic gyroscope is designed to provide comparable performance to the VG910H1. It features similar angular rate range, bandwidth, size, and environmental specifications, making it suitable as a replacement in many inertial navigation and stabilization systems.
Fiber optic gyroscopes provide several advantages compared with mechanical gyroscopes and MEMS sensors:
These characteristics make FOG sensors ideal for navigation and guidance applications.
Fiber optic gyroscopes are widely used in:
Fiber optic gyroscopes offer several advantages for UAV systems:
These features make FOG sensors ideal for drone flight control and navigation systems.
Fiber optic gyroscopes generally provide:
MEMS gyroscopes are usually smaller and lower cost but are often used in lower-precision navigation systems.
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