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3 axis gyroscope sensor (189) Online Manufacturer

Inertial Navigation Systems Electronic Gyroscope Sensor Based On Optical Sagnac Effect

Dimensions (mm): 98×98×35

Start Time (s): 5

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Three axis fiber optic gyroscope for flight attitude detection Digital output and weight ≤320(g)

Dimensions: 71.5×68×45 (mm)

Start Time: 3(s)

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weight ＜130g Light Weight Inertial Optical Gyroscope For Unmanned Aerial Vehicles，Operate temperature -45℃～+70℃

Scale Factor Non-linearity (ppm): ≤10

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

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MEMS gyroscopes are used for aircraft guidance and control,Size 4330.530.5(mm)，Weight ≤50(g)

Mean Time Between Failures(MTBF): 100000h

Bandwidth(Hz)can Customize: ≤100

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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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Low power precision mems gyroscope Scaling factor 3.3±0.05(mv/°/s), Cross coupling ≤2(%)

Output Voltage: 0.66～2.64(V)

Cross Coupling: ≤2(%)

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Fiber optic gyroscopes, angular velocity sensors for inertial systems with Dynamic range ±900(°) / s ,Random walk≤0.01

Supply Voltage (V): +5

Bias Drift (°) / H (10s Smooth) -45~ + 70℃: ≤0.3

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0.5-4.5(V) Analog Output MEMS Gyroscope With ≤20(Ms) Quick Run-Up Time

Output Noise: <0.02(°/s√Hz)

Operating Temperature Range: -45～+80(°C)

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Three-axis general purpose gyroscope with small size, operating temperature range -45 ~ +105(°C), zero-bias stability 1

Operating Temperature Range: -45～+105(°C)

Cross Coupling: ≤2(%)

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Airborne fiber optic gyroscope is used for attitude detection with Bias drift ≤0.1(°)/h and ±500 (°)/s Dynamic range

Operating Temperature: -45～+70(℃)

Dynamic Range: ±500 (°) / 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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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 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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High precision and high performance gyroscope for inertial navigation system with Random walk ≤0.0003(º/h^1/2)

Storage Temperature Of: -50～+80(℃)

Bias Repeatability: ≤0.001(°/h)

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High Precision Fiber optic gyroscopes for Inertial Navigation Systems (INS) Bias repeatability≤0.001(°/h)

Bias Repeatability: ≤0.001(°/h)

Scale Factor Non-linearity: ≤5(ppm)

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<6W Steady-state Power High precision low offset gyroscope ≤0.001°/H Bias Drift

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

Scale Factor Repeatability: ≤5ppm

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