Electronic Gyroscope Sensor

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High Performance Mems Gyroscope With ≤1.1(W) Power Dissipation And Vibration 6.06(G)

Operating Temperature: -40℃～+80(℃)

Nonlinearity: ≤0.02(%FR)

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Advanced Visual Inertial Navigation System For Aircraft Takeoff And Landing With Weight ≤2.0kg

Field Of View(visible Light): 57.80°×34.50°

System Preparation: Static Base Alignment, Alignment Time 5 Minutes

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Robust Inertial Navigation System Installation Dimensions 160mm X 150mm Host ≤ 12.5kg

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

Weight: Host ≤ 12.5kg

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Precision Electronic Gyroscope Sensor For Navigation ≤0.005º/H^1/2 Random Walk Coefficient

Storage Temperature Of: -45～+80℃

Weight (g): <550

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High Precision Low Offset Fiber Optic Gyroscope For Military Navigation

Bias Drift(10s Smooth) -45~ + 70℃: ≤0.003°/H

Supply Voltage: ±5V

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High Precision Electronic Gyroscope Sensor With Bandwidth 500Hz Bias Repeatability ≤0.5/≤1°/H

Resistance Of Insulation(MΩ): ＞100MΩ

Zero Bias Repeatability（1，10s） (°/h): ≤0.5/≤1°/h

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RS422 Electronic Gyroscope Sensor With Shock Resistance Of 5000(G) And ±500 ゜/S Range

Nonlinearity: ≤0.05(%FR)

Bias Repeatability: ≤0.05(゜/s)

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High Precision Mems Gyroscope With ≤0.05(゜/S) Bias Repeatability And ≤±0.1(゜/S) Bias

Size: 45×39×20(mm)

Operating Temperature: -40℃～+80(℃)

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50(g) Weight Mems Gyro Sensor With Range ±500(゜/s) for Industrial Applications

Size: 45×39×20(mm)

Storage Temperature: -55~+85(°C)

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Nonlinearity Of ≤0.1(%Fs) And 10000(g) Shock Resistance In MEMS Three Axis Gyroscope Sensor

Nonlinearity: ≤0.1(%Fs)

Bias Repeatability: ≤0.15(゜/s)

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MEMS Three Axis Gyroscope are used in inertial navigation systems with Range is ±300(゜/s) and shock 10000g

Shock: 10000(g)

Bandwidth: ≥90(Hz)

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Lightweight And Small Size Mems Three Axis Gyroscope With Size Is ф39.5×28.5(Mm) And Weight Is 100(G)

Weight: 100(g)

Bias Stability: 12(゜/h)

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MEMS Three Axis Gyroscopes For UAV Weight Less Than 100(g) With RS422 Electrical Interface

Bias Repeatability: ≤0.15(゜/s)

Cross Coupling: ≤1(°/s)

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Lightweight and high precision AI vision inertial navigation system for UAVs with Field of view(infrared) 35.83°×27.26°

Field Of View(infrared): 35.83°×27.26°

Length*width*height: 179mm×140mm×126mm

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Inertial navigation system for flight monitoring with accuracy (2σ) Level: 6m, Elevation: 8m

Dimensions: 160mm X 150mm X 56mm

Weight: Host ≤ 12.5kg

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High Torque First Stage Servo Mechanism For Rocket Control And Missile Guidance

Maximum Load Moment: ≥ 40000N·m

Maximum Output Power: ≥ 40kW

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