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gyroscope sensor module (155) Online Manufacturer

Data Rate Mems Gyroscope Gyroscope In Mems RS422 Interface Long MTBF Wide Temp Range

Data Updating Rate(can Set): 2000(Hz@460800)

Zero-bias: ≤±0.05(In 500°/s)(deg/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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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 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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<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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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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Low power triaxial angular rate gyroscope, can be applied to robots, Storage temperature -65 ~ +125(°C), Weight ≤40(g)

Offset Voltage: 2.5±0.05(V)

Resolution/Threshold: ≤0.1(°/s)

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Customizable Bandwidth 80Hz Mems Gyroscope Mems Gyro Wide Temp Range -45～+80(°C) Nonlinearity ≤0.05(%FR)

Bandwidth Can Customize: 80(Hz)

Nonlinearity: ≤0.05(%FR)

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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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Fiber optic gyroscopes for aircraft navigation and platform stability testing with ≤0.01(°) / H Bias drift

Operate Temperature: -40～+70℃

Scale Factor Repeatability: ≤10ppm

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Triaxial angular rate gyroscope Operating temperature range -45~+80℃,G-value sensitivity <0.02(°/s/g)

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

Incoming CurrentmA: <30 MA

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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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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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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 gyroscopes have a wide range of operating temperatures -40～+70℃ and ±300(°) / S Dynamic range

Supply Voltage: ±5V

Start Time: ≤5s

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MEMS sensors can be used for missile guidance and control, and the size is small, suitable for RS422, weight ≤50 (g)

Power: DC5(V)

Mean Time Between Failures: 10(Kh MTBF)

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