Starts from the Best Quality

Super high performance single-axis fiber gyroscope, bias stability ≤0.005°/h (room temperature), has been widely used in tactical grade applications.

• Super High Performance Digital Fiber Optic Gyro
• Higher Accuracy, Lower Noise and Greater Efficiency
• Zero Bias Stability ≤ 0 .005 °/h (Normal Temperature)
• Zero Bias Stability at Full Temperature ≤0.02°/h
• Measuring Range: -300°/s~+300°/s
• Scale Factor Non-linearity ≤10ppm
• Bandwidth ≥200Hz
• Working Temperature: -40~+60ºC

High performance single-axis fiber optic gyro, bias stability ≤0.05°/h (room temperature), has been widely used in tactical grade applications.

• Super High Performance Digital Fiber Optic Gyro
• Higher Accuracy, Lower Noise and Greater Efficiency
• Zero Bias Stability ≤ 0 .007 °/h (Normal Temperature)
• Zero Bias Stability at Full Temperature ≤0.02°/h
• Measuring Range: -300°/s~+300°/s
• Scale Factor Non-linearity ≤10ppm
• Bandwidth ≥200Hz
• Working Temperature: -40~+60ºC

high performance single-axis digital optical gyro, bias stability ≤0.05°/h (room temperature), has been widely used in tactical grade applications.

• High Performance Single Axis Fiber Optic Gyro
• Higher Accuracy, Lower Noise and Greater Efficiency
• Zero Bias Stability ≤ 0.05°/h (Room Temperature)
• Zero Bias Stability at Full Temperature ≤0.1°/h
• Measuring Range: -400°/s~+400°/s
• Scale Factor Non-linearity ≤50ppm
• Bandwidth ≥200Hz
• Working Temperature: -40~+70ºC

high performance single axis fiber optic gyroscope, bias stability at fixed temperature ≤0.2°/h, widely used in navigation, and precision pointing, etc.

• High Performance Single Axis Fiber Optic Gyro
• Higher Accuracy, Lower Noise and Greater Efficiency
• Measuring Range: -700°/s~+700°/s
• Zero Bias Stability ≤ 0 .2°/h (Room Temperature)
• Zero Bias Stability at Full Temperature ≤0.5°/h
• Scale Factor Non-linearity ≤100ppm
• Bandwidth ≥200Hz
• Working Temperature: -40~+70ºC

high performance fiber optic gyro, bias stability at fixed temperature ≤0.1°/h (1σ), has been widely used in motion sensing, stabilization, etc.

• High Performance Single-axis Digital Fiber Optic Gyro
• Higher Accuracy, Lower Noise and Greater Efficiency
• Measuring Range: -600°/s~+600°/s
• Bias Stability at Fixed Temperature ≤0.1°/h (1σ)
• Bias Repeatability at Full Temperature ≤0.3°/h (1σ)
• Scale Factor Non-linearity ≤50ppm
• Bandwidth ≥200Hz
• Working Temperature: -40~+70ºC

high-performance solid state gyro, bias stability at fixed temperature ≤0.5°/h (1σ), widely used in motion sensing, stabilization, navigation, etc.

• High Performance Single-axis Digital Fiber Optic Gyro
• Higher Accuracy, Lower Noise and Greater Efficiency
• Measuring Range: -800°/s~+800°/s
• Bias Stability at Fixed Temperature ≤0.5°/h (1σ)
• Bias Repeatability at Full Temperature ≤0.5°/h (1σ)
• Scale Factor Non-linearity ≤300ppm
• Bandwidth ≥100Hz
• Working Temperature: -40~+70ºC

High performance closed-loop digital fiber optic gyro, widely used in attitude control, inertial navigation and integrated navigation, etc.

• High Performance Digital Fiber Optic Gyro
• Higher Accuracy, Lower Noise and Greater Efficiency
• Zero Bias Stability ≤ 0.2 °/h (Fixed Temperature)
• Zero Bias Stability at Full Temperature ≤0.5°/h
• Measuring Range: -400°/s~+400°/s
• Scale Factor Non-linearity ≤50ppm
• Bandwidth ≥200Hz
• Working Temperature: -40~+60ºC

highly precise attitude determination system, based on 4 groups of GNSS receivers, widely used in the surface craft.

• Built-in Mini AHRS soft/hardware
• Yaw, Roll, Pitch, Acceleration and Angular Rate Outputs
• High Accuracy: Yaw: 0.2° , Attitude: 0.1° (base line≥1m)
• RS232/RS422 Interface, 100Hz /200Hz Output Rate
• High Reliability, Strong Vibration and Shock Proof
• Advanced SkyMEMS Data Fusion Algorithm
• Wide Operating Temperature: -40°C～+85°C

high-performance airborne GPS aided inertial system, widely used in unmanned aircraft, vehicle navigation, surface craft, ship, and so on.

• High-Performance MEMS Inertial System with GPS/GLONASS Satellite Navigation System
• High Accuracy: Yaw: 0.5° (1σ), Attitude: 0.23° (1σ), Velocity <0.05~0.1m/s, Position < 5m (L1/L2 single point), <8cm (RTK), Heave: <15cm (1σ)
• RS422 Interface, 100Hz Data Output Rate
• High Reliability, Strong Vibration Proof
• Advanced SkyMEMS Data Fusion Algorithm

High Performance rugged GNSS aided inertial system, widely used in tactical weapon, unmanned aerial vehicle (UAV), ship, etc.

• 3 Systems, 6 Frequency GNSS
• High Tracking Sensitivity for Complicated Environment
• High Accuracy: yaw up to 0.1°, Attitude: 0.1° (rms), Velocity <0.03m/s, Position < 0.01m (RMS, RTK),
• High Reliability, Strong Vibration and Shock Resistance
• Multiple Interfaces: RS232 / RS422 /TTL
• Adjustable Bandwidth and Protocol ODM Supported

High precision integrated navigation system, widely used in unmanned aerial vehicle (UAV), vehicle navigation, the surface craft, ship and so on.

• High Precision MEMS Inertial System with GPS/BD Dual-mode Satellite Navigation System
• High Accuracy: Heading: 0.15°(rms), Attitude: 0.05° (rms), Velocity <0.15m/s, Position < 1.5m
• Support Dynamic Fast Alignment
• High Reliability, Strong Vibration and Shock Resistance
• Multiple Interfaces: RS232/RS422/TTL/CAN
• Easy to Integrate with Odometer/DVL Sensor

GINS100 Embedded GPS Inertial Navigation System

– Low-Cost MEMS GNSS/INS System with GPS/BeiDou

Dual-mode Satellite Navigation System

– High Accuracy: Yaw: 0.5° (RMS), Attitude: 0.5° (RMS)

Velocity <0.15m/s, Position < 5m (RMS)

– Up to 400Hz Output Rate

– High Reliability, Strong Vibration Proof

– Small Size: 43 × 37× 15mm, 20grams (without casing)

– Wide Operating Temperature: -40°C～+70°C

High Precision analog output inertial measurement unit, 3000g high overload resistance, widely applied in precision weapon, etc.

• High Precision Military 6 DoF Mini IMU
• 3 Angular Rates and 3 Linear Acceleration as well as Rotation Rate Outputs
• Data Output Rate: 100Hz
• Range: Gyro (X axis) ±20000°/s, Accel ±100g
• High Overload Resistance: 3000g
• Compact and Light weight D40*25mm, <90grams

High Overload Resistance 10000g MEMS Inertial Measurement Unit, widely applied in precision weapon, rocket, etc.

• High Stability, High Reliability, High Accuracy, High Survivability in Harsh Environment, Fully Calibrated
• Angular Range:±150°/s, Acceleration Range：±10g (Supporting Custom Design)
• Bias Stability: Gyro 30°/h, Acc 1mg (1σ)
• Overload Resistance:10000g, IP67 Protection
• Wide Temperature: -40°C～+85°C
• Compact Size: 38*35*28mm

Precision MEMS inertial measurement unit, compatible with ADIS16488A, widely applied in tactical UAS navigation, precise guided bomb, rocket, etc.

• Precision 6 DoF MEMS Inertial Measurement Unit
• Compatible with ADIS16488A Interface and Protocol
• Dynamic Range: Gyro ±450°/s, Acc ±16g
• Bias Instability: Gyro: 0.8°/h, Acc 0.03mg (Allen)
• Ability to Access with GNSS, Aerospace Reliability
• Full Temperature Range Accuracy: Built-in High
• Performance Temperature Calibration and Compensation Algorithm

High precision 6 DoF mems angular rate sensor, full calibration, widely applied in unmanned aircraft, automatic vehicles and ROVs, AGV, etc.

• High Precision 6 DoF MEMS IMU with Full Calibration
• 7 Sensor Outputs: angular rate (x3), linear acceleration (x3), and temperature; Data Output Rate: up to 1000Hz
• Range: Gyro ±500°/s, Acc ±10g, (more options)
• Bias Instability: Gyro 5°/h, Acc 0.03mg (Allan Variance)
• IP67 Protection, Voltage: 5V or 9~36VDC
• Compact and Light weight – 50 x 45 x 21 (mm), 70grams
• Wide Working Temperature: -40°C～+85°C