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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 dengan antarmuka RS422 Anti-Interferensi untuk Kontrol Tingkat Platform

Tegangan masukan (Vdc): 7,5 ~ 32Vdc

Jangkauan pengukuran (°): ± 15 ~ ± 90

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Sensor Gyro Sumbu Tunggal 200Hz dengan Stabilitas Bias Tinggi dan Output RS422 untuk Pengukuran Presisi

Tegangan masukan: 6±0,1VDC

Masukan Saat Ini: ≤150mA

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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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Giroskop Optik Inersia Ringan

Non-linearitas faktor skala (ppm): ≤10

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

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Sensor Giroskop Serat Optik dengan Suhu Operasional -45~+70℃ ±500°/s Rentang Dinamis dan Bias Drift ≤0,5°/jam

Penyimpangan bias (10 detik halus) -45~ + 70℃: ≤0,5(°/jam)

Pengulangan faktor skala: ≤10 (ppm)

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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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