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Electronic Gyroscope Sensor

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Optical angular velocity sensors are used in aerospace, Dynamic range ±900 (°) / s,weight <130(g)

Dimensions (mm): 50×50×36

Random Walk Coefficient(º)/h^1/2: ≤0.01

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Three axis fiber optic gyroscope for IMU with Bias drift ≤0.1(°) /h and weight<320(g)

Dimensions: 71.5×68×45(mm)

Bias Drift(10s Smooth, Fix Temperature): ≤0.1(°)/h

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High precision gyroscope detects angular velocity in real time with weight <130g and Dimensions

Operate Temperature ℃: -45~+70℃

Supply Voltage (V): +5

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Integrated inertial navigation system for communication and navigation of UAVs with Installation dimensions 160mm X 150m

Installation Dimensions: 160mm X 150mm

Data Link Working Frequency Band: 3.4GHz~3.6GHz

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KSGYR104F Fibre Optic Gyroscope ±500°/s 70×70×32mm

Supply Voltage: +5V

Dimensions: 70×70×32 Mm

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Bias Drift ≤0.1°/H Gyro North Finder with ±5V Supply Voltage for Accurate Navigation and Uav

Steady-state Power Consumption (full Temperature): <3W

Weight (g): <550

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State-of-the-Art Inertial Navigation System Aviation for Aviation Applications with Navigation accuracy (takeoff) 1.0m

Navigation Accuracy (takeoff): 1.0m

Navigation Accuracy (cruise): 20m+1%H

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Advanced Inertial Navigation System Aviation with Power Requirement 18V-36V DC

Data Output Frequency: 10Hz (typical)

Input/output Interface: 2 RS-422, 1 RS-232, 1 100M Ethernet

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High-Performance Inertial Navigation System with Digital input/output RS-422,RS-232 and 100M Ethernet

Spatiotemporal Synchronization Accuracy In Case Of Satellite Rejection (RMS): 5m/5ns

Dynamic Range: Speed: -2000m/s ~ 2000m/s; Acceleration: -30g ~ 30g; Acceleration: -5g/s ~ 5g/s.

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Digital quartz MEMS gyroscope chip Scale factor So 70 LSB/(°/s) ±2% and Current consumption Iop1 900μA Typ

Operating Temperature TOPR: -20℃~+80℃

Bias Variation Over Temperature B ZRLtb: ±1°/h

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MEMS gyroscope sensor for automotive electronics, output voltage 0.66~2.64 V, zero-bias stability of 12°/h

Output Voltage: 0.66~2.64(V)

Bandwidth(Hz)can Customize: ≤100

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Long-life Output voltage of stable three-axis MEMS gyroscope sensor is 0.66 ~ 2.64 v, Output noise ≤0.02(°/s/g)

G-value Sensitivity: ≤0.02(°/s/g)

Output Noise: ≤0.02(°/s√Hz)

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