Sensor Giroskop Elektronik

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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)

Dapatkan Harga Terbaik

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℃

Dapatkan Harga Terbaik

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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High Precision Biaxial Fiber Rotating Inertial Navigation System Multiple Modes For Large UAVs

Align time: Normal alignment on the ground: ≤ 13min

Position Accuracy (CEP): Pure inertia: 1nmile/12h

Dapatkan Harga Terbaik

Optical Fiber Rotating Inertial Navigation System For UAV Flight Control And Navigation And Positioning

Align time: Normal alignment on the ground: ≤ 5min

Position Accuracy (CEP): Pure inertia: 1.5 nmile/6h After 15min of inertial/satellite combination: 1.0 nmile/6h Inertia/satellite combination: ≤ 10m

Dapatkan Harga Terbaik

Integrated Flight Control Inertial Navigation Equipment For High Speed UAVs

Align time: 270s

Position accuracy: ≤ 1nmil（1σ,1h）

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Small Volume Strapdown Inertial Navigation System Uses Optical Fiber Gyroscope For UAV

Align time: ≤5min

Speed accuracy: In integrated navigation mode: sky speed ≤ 0.3m/s, horizontal speed ≤ 0.2m/s

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