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Fast Start Analog Output MEMS Gyroscope Sensor With Offset Voltage Of 1.65±0.02(V)

Weight: ≤50(g)

run-up time: ≤5(ms)

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Weight≤50(G) Three Axis MEMS Gyroscope Sensor For Industrial

Range: ±300(°/s)

run-up time: ≤5(ms)

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Mems Gyro Sensors For Robot Or Camera Stabilization Systems With Size 43x30.5x30.5mm And Weight ≤50(G)

Output noise: <0.02(°/s√Hz)

Operating temperature range: -45~+105(°C)

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Precise Industrial Measurements Electronic Gyroscope Sensor With ≤2(%) Cross Coupling

G-value sensitivity: <0.02(°/s/g)

Bandwidth: ≤100(Hz)

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High Performance Mems Gyroscope With ≤1.1(W) Power Dissipation And Vibration 6.06(G)

Operating temperature: -40℃~+80(℃)

nonlinearity: ≤0.02(%FR)

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Advanced Visual Inertial Navigation System For Aircraft Takeoff And Landing With Weight ≤2.0kg

Field of view(visible light): 57.80°×34.50°

System preparation: Static Base Alignment, Alignment Time 5 Minutes

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Robust Inertial Navigation System Installation Dimensions 160mm X 150mm Host ≤ 12.5kg

Dynamic Range: Speed: -2000m/s ~ 2000m/s; Acceleration: -30g ~ 30g; Acceleration: -5g/s ~ 5g/s.

weight: Host ≤ 12.5kg

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Precision Electronic Gyroscope Sensor For Navigation ≤0.005º/H^1/2 Random Walk Coefficient

Storage temperature of: -45~+80℃

weight (g): <550

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High Precision Low Offset Fiber Optic Gyroscope For Military Navigation

Bias drift(10s smooth) -45~ + 70℃: ≤0.003°/H

Supply voltage: ±5V

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High Precision Electronic Gyroscope Sensor With Bandwidth 500Hz Bias Repeatability ≤0.5/≤1°/H

Resistance of insulation(MΩ): >100MΩ

Zero bias repeatability(1,10s) (°/h): ≤0.5/≤1°/h

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RS422 Electronic Gyroscope Sensor With Shock Resistance Of 5000(G) And ±500 ゜/S Range

nonlinearity: ≤0.05(%FR)

Bias repeatability: ≤0.05(゜/s)

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High Precision Mems Gyroscope With ≤0.05(゜/S) Bias Repeatability And ≤±0.1(゜/S) Bias

Size: 45×39×20(mm)

Operating temperature: -40℃~+80(℃)

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High Torque First Stage Servo Mechanism For Rocket Control And Missile Guidance

Maximum load moment: ≥ 40000N·m

Maximum output power: ≥ 40kW

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Inertial Satellite Integrated Navigation System For Unmanned Vehicles And Drones And Missiles

Alignment time (min): 1min~5min

weight: ≤ 130g (excluding antenna )

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Fiber Strapdown Inertial Navigation System For High Altitude Airships And Fixed Wing UAVs

Align time: ≤5min

Working/storage temperature(℃): -40℃ ~+60℃ /-45℃ ~+80℃

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Miniature Inertial Navigation System With High Precision Fiber Optic Gyro For UAV Navigation

Align time: ≤5min

heading alignment accuracy: ≤ 0.06° (1σ) (self-aligned)

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