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MEMS Integrated Navigation System GNSS INS for UAV Drone Positioning and Attitude Measurement

MEMS Integrated Navigation System GNSS INS for UAV Drone Positioning and Attitude Measurement

The I3200 micro-integrated navigation system is a compact and cost-effective MEMS-based integrated navigation system, primarily targeting the fields of navigation, control, and measurement represented by mobile communication and unmanned aerial vehicles. The system highly integrates MEMS sensors and full-frequency satellite receiver chips within a small size, enabling positioning and attitude measurement in a compact package.

  • Part No, :

    I3200
  • Order(MOQ) :

    1
  • Description

Product Series and Parameters

Parameter Technical Indicators
Gyroscope
Range(°/s) ±300
Full-temperature zero bias(°/h,3σ) ≤360
Zero bias stability(°/h,10s ) ≤10
Zero bias instability(°/h,allan,typ) ≤3
Zero bias repeatability(°/h) ≤10
Angle random walk(°/√h) ≤0.3
Scale factor nonlinearity(ppm) ≤100
Axis cross-coupling(rad) ≤0.001
Bandwidth(Hz) ≥100
Accelerometer
Range(g) ±16
Full-temperature zero bias(mg,3σ) ≤5
Zero bias stability(μg,10s) ≤300
Zero bias instability(μg,allan,typ) ≤50
Zero bias repeatability(ug) ≤300
Velocity Random Walk(m/s/√h) ≤50
Scale factor nonlinearity(ppm,±1g) ≤300
Axis cross-coupling(rad) ≤0.001
Bandwidth(Hz) ≥100
Navigation Accuracy
Combined horizontal position (m, 1σ) 3m (single point)
0.02+1ppm (RTK)
Combined sky position (m, 1σ) 5m (single point)
 0.03+1ppm (RTK)
Combined horizontal speed (m/s, 1σ) 0.1
Combined skyward velocity (m/s, 1σ) 0.15
Combined heading (°, 1σ, real-time) 0.2 (1m baseline dual-antenna)
 0.5 (single antenna, dynamic)
Combined horizontal attitude (°, 1σ, real-time) 0.1° (dual-antenna)
0.2° (single-antenna)
Electrical/mechanical interface
Power supply (V) 5V
Steady-state power (W) ≤0.5
Startup time (s) ≤3
communication interface URAT
Update rate (Hz) 100
Size (mm×mm×mm) 41.5×35.5×9.5
Weight (g) <30
Operating Environment
Operating temperature(℃) -40~+80
Storage temperature(℃) -55~+85
Vibration(g,RMS) 20~2000HZ,6.06
Shock(g) 1000g/1ms
Reliability
MTBF(h) 10000

Production process


Product dimension

Inertial Navigation System

 


Application Scenarios

MEMS INS application
The MEMS-based INS (Inertial Navigation System) is suitable for navigation and motion control scenarios such as UAV/UGV autonomous navigation, vehicle/ship attitude measurement and GNSS/INS integrated navigation, antenna/camera stabilization platforms, and mobile mapping & positioning—providing compact size, low power consumption, fast start-up, and stable attitude/heading outputs for dynamic environments.
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FAQ

Q1. What is the I3200?
I3200 is a high-performance MEMS integrated inertial navigation system. It combines MEMS inertial sensors with a full-frequency GNSS receiver in a compact design, and is suitable for navigation, control, and measurement applications.

Q2. What are the main features of the I3200?
The I3200 features high performance, compact size, low weight, ultra-low power consumption, full-temperature calibration compensation, optional adaptive attitude algorithm, lever arm compensation, software online upgrade, GNSS-denied self-correcting attitude capability, and RTK integration support.

Q3. What applications is the I3200 suitable for?
The I3200 is suitable for communication on the move, position and attitude reference for drones, vehicles, ships, and boats, attitude control, and other unmanned system applications.

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