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Electronic Gyroscope Sensor

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Gyroscope Sensor for Precision Flight Testing 460800bps 6.06 G Vibration Tolerance

Bias Stability: ≤0.002g

Operating Temperature: -40~+65℃

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Fiber Optic Gyroscope For Oil Drilling Platform With -45~+70 (℃) Operate Temperature ±500(°/s) Dynamic Range

Dimensions: 60×60×32(mm)

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

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Digital Quartz MEMS Gyroscope Chip Operating Temperature TOPR -20℃ ~ +80℃, Current Consumption Iop1 900μA Typ

Rate Range I: ±400°/s

Scale Factor So: 70 LSB/(°/s) ±2% 17920 LSB/(°/s) ±2%

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Cross-axis Sensitivity CS±5% And Supply Voltage 2.7V~+3.6V Digital Quartz MEMS Gyro Temperature Control Sensor

Supply Voltage: +2.7V~+3.6V

Scale Factor Variation Over Temperature Spt: ±3%

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High Precision Fiber Optic Gyroscopes Used In Inertial Measurement Instruments

Dimensions (mm): 120×120×38

Start Time (s): 5

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Digital RS422 Output Interface Electronic Gyroscope Sensor For Automotive Applications

Supply Voltage: 5DC±5%V

Shock: 8000 G , 0.5 Ms, 1/2 Sine

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KTG-50 land strapdown system dynamic tuning gyroscope

Random Drift: ≤0.01°/h

Power(1 Phase): 5&16000V & Hz

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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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Drones Inertial Navigation Systems Based On Fiber Optic Gyroscopes with power consumption ≤ 20W

Power Consumption: ≤ 20W

Operating Temperature: -40℃~ +65℃

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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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Fixed Wing UAV Iaser Strapdown Inertial Navigation System with dimensions 185mm×139.5mm×110mm

Position Accuracy: 0.5nmile/h(CEP)

Speed Accuracy: 0.5m/s(RMS)

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AI vision inertial navigation system for aircraft lifting assistance with weight ≤2.0kg

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

Storage Temperature: -45℃ ~+65℃

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