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Harga yang bagus Well Logging Dynamically Tuned Gyroscope For High Temperature Environment on line Video

Well Logging Dynamically Tuned Gyroscope For High Temperature Environment

Suhu: -15 ~ 100 ℃

Getaran: 5g

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Inertial Navigation Systems Electronic Gyroscope Sensor Based On Optical Sagnac Effect

Dimensions (mm): 98×98×35

start time (s): 5

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Metal Shell Mems Gyro Sensor Anti Interference With Platform Level Control

Input voltage (Vdc): 7.5 ~ 32Vdc

Measuring range (°): ± 15 ~ ± 90

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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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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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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 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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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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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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Berat <130g Berat Ringan Giroskop Optik Inersia Untuk Kendaraan Udara Tanpa Awak,Suhu operasi -45°C+70°C

Non-linearitas faktor skala (ppm): ≤10

Koefisien berjalan acak ((o) / h ^ 1/2: ≤0,01

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

Mengoperasikan Suhu: -40~+70℃

Pengulangan faktor skala: ≤10ppm

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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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MEMS gyroscopes are used for aircraft guidance and control,Size 43*30.5*30.5(mm),Weight ≤50(g)

Mean time between failures(MTBF): 100000h

Bandwidth(Hz)can customize: ≤100

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