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Mems High Precision Integrated Navigation System Gnss/Ins Fusion for Unmanned Vehicle and Ship

Mems High Precision Integrated Navigation System Gnss/Ins Fusion for Unmanned Vehicle and Ship

I4500 integrated navigation system has built-in high-performance MEMS gyroscope and accelerometer, which can receive external GNSS data, realize multi-sensor fusion and integrated navigation algorithm, and have short-term inertial navigation capability when GNSS is invalid.

The product has high reliability and strong environmental adaptability. By matching different software, the products can be widely used in the fields of tactical and industrial unmanned aerial vehicles, unmanned vehicles, unmanned ships, aviation guided bombs, intelligent ammunition, rockets, mobile communication, mapping, seeker and stable platform.

The product is divided into low-configuration version (I4500-A) and high-configuration version (I4500-B). The two products have different precision and price, which is convenient for users to choose based on specific use conditions.

  • Part No, :

    I4500
  • Order(MOQ) :

    1
  • Description

Product Series and Parameters

  Project Metrics (RMS) Remark
Heading accuracy Dual GNSS 0.1° 2m baseline
Single GNSS 0.2° Need to maneuver
GNSS failure retention accuracy 0.2°/min I4500-B
0.5°/min I4500-A
Attitude accuracy GNSS is valid 0.1° I4500-B
0.2° I4500-A
GNSS failure retention accuracy 0.2°/min I4500-B
0.5°/min I4500-A
V-G mode(GNSS failure time unlimited, no acceleration) I4500-B
I4500-A
Horizontal positioning accuracy GNSS is valid 1.2m Single point L1/L2
2cm+1ppm RTK
GNSS failure (60s) 20m I4500-B
100m I4500-A
Horizontal velocity accuracy GNSS is valid 0.1m/s Single point L1/L2
Gyroscope Measuring range ±450°/s  
Zero-bias stability (Allan variance) 2°/h I4500-B
4°/h I4500-A
Measuring range ±16g Customizable 200 G
Accelerometer Zero-bias stability (Allan variance) 30µg I4500-B
60µg I4500-A
Communication interface UART Route 2  
PPS Route 1 Input, LVTTL
SPI Route 1  
Electrical characteristics Voltage 3~3.6VDC  
Power consumption ≤1.5W  
Ripple 100 mV P-P
Structural characteristics Size 47 mm×44 mm×14mm  
Weight ≤50g  
Use environment Operating temperature -40℃~+70℃  
Storage temperature -45℃~+75℃  
Vibration 20~2000Hz,6.06g  
Impact 1000g,0.5ms  
Reliability MTBF 20000h  
Life span > 15 years  
Continuous working time >120h  

Production process


Product dimension

INS

 


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 are the main versions of the I4500?
A: I4500-A: Lower-cost version with slightly reduced accuracy.
I4500-B: High-performance version with superior accuracy.

Q2: What are the typical applications?
A: Unmanned Aerial Vehicles (UAVs)
Unmanned Ground Vehicles (UGVs)
Unmanned Surface Vessels (USVs)
Guided munitions, rockets, smart ammunition
Mobile communications, mapping, seeker and stabilization platforms
 
Q3: What are the key performance specifications?
A: Gyroscope Bias Stability: 2°/h (I4500-B), 4°/h (I4500-A)
Accelerometer Bias Stability: 30 µg (I4500-B), 60 µg (I4500-A)
Heading Accuracy: 0.1° (dual GNSS), 0.2° (single GNSS)
Positioning Accuracy: 1.2m (single point), 2cm+1ppm (RTK)
Power Consumption: ≤1.5W
Operating Temperature: -40°C to +70°C
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