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Inertial Angular Rate Sensor Based On Optical Sagnac Effect Use In Measure Angular Velocity，start time 5(s)

Dimensions: 50×50×36(mm)

Start Time: 5(s)

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Inertial Angular Velocity Sensor For Photoelectric Pod Flight Control Platform

Start Time (s): 5

Dimensions (mm): 70×70×32

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Gyroscope/Angular velocity sensor/Used to measure the angular velocity in the direction of the sensitive axis

Dimensions (mm): 98×98×35

Start Time (s): ≤5

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High Precision Gyroscope / Angular Velocity Sensor Used In Aerospace Scientific Experiments

Dimensions (mm): 120×120×38

Start Time (s): 5

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UAVs Collaborative Navigation System Integrates Communication And Navigation

Satellite Positioning Accuracy (2σ): Level: 6m, Elevation: 8m

Communication Distance: 100km

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Airborne Inertial Visual Navigation System For Unmanned Aerial Vehicles Or Aircraft

Action Range: 1km~8km

Navigation Accuracy: 1.0m(1σ,lateral Accuracy)/20m+1%H (1σ, Horizontal Positioning Accuracy,H Is The Height Of The Aircraft Relative To The Ground)

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UAV Small MEMS Inertial Measurement Unit Integrating Three Gyroscopes And Accelerometers

Angular Rate Measurement Range (°/s): 400

Acceleration Measurement Range (g): 50

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Optical Fiber Strapdown Inertial Navigation System For Large UAVs Flight Control

Align Time: ≤5min

Position Accuracy: Pure Inertia: 0.8nmile/h (CEP); Integrated Navigation With Satellite: Altitude 10m; Level 5m

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Integrated Flight Control Inertial Navigation Equipment For High Speed UAVs

Align Time: 270s

Position Accuracy: ≤ 1nmil（1σ,1h）

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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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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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Optical Fiber Strapdown Inertial Navigation System For High Altitude Airships And Large Unmanned Aerial Vehicles

Align Time: ≤5min

Heading Alignment Accuracy: ≤ 0.06° (1σ) (self-aligned)

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Integrated Navigation Processing Equipment For Missile Launch Reference,Power consumption ≤ 100W

Power Consumption: ≤ 100W

Weight: 10kg

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Lidar Cloud Map Matching And Environment Sensing Devices For Driverless Car Navigation

Location (CEP): 10m

Preparation Time: 5min

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High-temperature acceleration sensors are used for LogPlot plotting and well logging

Scope: ±30g

Installation Error: ＜1500µrad

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Vibration Resistance Quartz Flexible Accelerometers Used For Bridge And Well Drilling Inclination Measurements

Scope: ±30g

Installation Error: ＜1500µrad

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