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Electronic Gyroscope Sensor

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High precision UAV gyroscope Used in flight control system with Random walk ≤0.0003(º/h^1/2) and Bias drift ≤0.001(°/h)

Random Walk Coefficient: ≤0.0003(º/h^1/2)

Scale Factor Repeatability: ≤5(ppm)

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High precision gyroscopes are used in aerospace fields with Dimensions 120×120×38(mm) Weight<1000(g)

Bias Drift(10s Smooth, Fix Temperature): ≤0.001(°/h)

Scale Factor Non-linearity: ≤5(ppm)

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High-Performance Gyroscope Sensor for Accurate Angular Velocity Measurement With ≤0.001(°/h)

Storage Temperature Of: -50~+80(℃)

Scale Factor Non-linearity: ≤5(ppm)

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Highly Accurate and ≤0.005º/h^1/2 Low Random Walk Coefficient Electronic Gyroscope Sensor

Scale Factor Repeatability: ≤10ppm

Dynamic Range: ±300(°) / S

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High-performance motion tracking with Electronic Gyroscope Sensor with ≤0.005º/h^1/2 Random walk coefficient

Random Walk Coefficient: ≤0.005(º)/h^1/2

Dimensions: 98×98×35mm

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High precision fiber optical Sagnac effect gyroscope with Random walk coefficient ≤0.005º/h^1/2

Bias Repeatability: ≤0.03(°) / H

Scale Factor Non-linearity: ≤10ppm

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Highly Sensitive Electronic Gyroscope Sensor Dimensions 98×98×35mm

Dynamic Range: ±300(°) / S

Storage Temperature Of: -45~+80℃

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Optical gyroscopes and angular velocity sensors are used in the IMU with ±300(°) / S Dynamic range

Storage Temperature Of: -45~+80℃

Dynamic Range: ±300(°) / S

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Fiber optic gyroscopes for inertial navigation systems with Random walk coefficients ≤0.01(°/h1/2) and RS422

Operate Temperature: -45~+70 (℃)

Steady-state Power Consumption (full Temperature): <4 (W)

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Miniaturized three-axis fiber optic gyroscope with RS422 Interface

Dimensions: 71.5×68×45 (mm)

Start Time: 3 (s)

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Automotive navigation grade fiber optic gyroscope with ≤0.1(°)/h Bias drift and weight≤320(g)

Start Time: 3(s)

Random Walk Coefficient: ≤0.01 (°)/h1/2

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High-precision three-axis FOG sensor for UAV navigation and IMU weight <320(g)

Dimensions: 71.5×68×45 (mm)

Start Time: 3 (s)

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