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Fiber Optic Gyro
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5v Fiber Optic Gyro Aircraft Inertial Navigation Systems Small Size

5v Fiber Optic Gyro Aircraft Inertial Navigation Systems Small Size

Brand Name: Firepower
Model Number: MFOG-24A
MOQ: 1
Payment Terms: T/T
Supply Ability: 200/MONTH
Detail Information
Production Name:
Navigation Gyro
Zero-bias Stability:
≤2°/h
Zero-bias Repeatability:
≤2°/h
Angular Random Walk:
≤0.04°/h
3dB Band Width:
≥450Hz
Power Supply:
5+0.15V
Packaging Details:
Sponge+ box
Supply Ability:
200/MONTH
Highlight:

5v Fiber Optic Gyro

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Aircraft Fiber Optic Gyro

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Aircraft Inertial Navigation Systems 70×70×32mm

Product Description
5V Fiber Optic Gyro Aircraft Inertial Navigation Systems Small Size
Engineered for high dynamic and harsh environments, the MFOG-24 Micro-Nano FOG combines compact structure, lightweight materials, and high shock resistance. It features no moving parts, minimal drift, and long operational life, supporting accurate attitude and heading data for UAVs and autonomous vehicles.
Key Specifications
Weight:
≤30g
Operating temperature:
-40℃ to +65℃
Storage temperature:
-55℃ to +85℃
Random vibration:
20g, frequency range: 20Hz to 2000Hz
Main Performance Parameters
Table 1: Main Performance Parameters
Serial number Project Performance indicators MFOG-24-AN
1 Range (°/s) ±500 ±300
2 Scale factor 3600(LSB/o/s) 7mv/o/s
3 Scale factor nonlinearity (ppm) 300 ≤1000
4 Zero-bias stability (10s, 1σ, °/h) ≤1.5 ≤2
5 Zero-bias repeatability (1σ, °/h) ≤1.5 ≤2
6 Angular random walk (°/h)1/2 ≤0.03 ≤0.04
7 Zero bias (°/s) ≤0.02 ≤0.05
8 3dB Band Width (Hz) ≥300 ≥450
9 Power supply (V) 5+0.15 5+0.15
10 Power Consumption (W) ≤1.5 ≤0.7
11 Dimension (mm) φ24X39
External Power Supply Requirements
Parameter Specification
Voltage 4.85V to 5.15V
Ripple 20mV
Electric current 0.2A