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Home » Unmanned System Products » China Moneypro MOPKT-EX9-3-A MEMS Attitude and Heading Reference System (AHRS) Module
China Moneypro MOPKT-EX9-2-A MEMS Attitude and Heading Reference System (AHRS) Module
China Moneypro MOPKT-EX9-2-A MEMS Attitude and Heading Reference System (AHRS) Module
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China Moneypro MOPKT-EX8-4N Single-Antenna Integrated Navigation System
China Moneypro MOPKT-EX8-4N Single-Antenna Integrated Navigation System

China Moneypro MOPKT-EX9-3-A MEMS Attitude and Heading Reference System (AHRS) Module

The system integrates a high-performance MEMS Inertial Measurement Unit (IMU) with proprietary attitude, heading, and geomagnetic fusion algorithms. By introducing a magnetometer error ellipsoid model, the system enables real-time online calibration of magnetic interference, ensuring stable and reliable output of angular velocity, acceleration, heading, and attitude data even in dynamic environments. It is widely used in navigation, control, measurement, positioning, and orientation applications.

Category: Inertial Navigation MEMS/IMU/Gyroscopes
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  • Description
Description

🚨 Industry Pain Points

In modern navigation and motion control applications, users often face several challenges:

  • Magnetic interference affecting heading accuracy
  • Sensor drift leading to unstable attitude data
  • Difficulty maintaining reliable output in dynamic environments
  • Complex calibration procedures for magnetometers
  • Low accuracy in navigation and positioning systems
  • Poor data stability in harsh industrial environments

These issues can significantly impact system accuracy, reliability, and operational performance.


⚙ Product Advantages

Our system is designed to overcome these technical challenges:

  • ✔ High-precision MEMS Inertial Measurement Unit (IMU)
  • ✔ Proprietary attitude, heading, and geomagnetic fusion algorithm
  • ✔ Magnetometer error ellipsoid model for improved heading accuracy
  • ✔ Real-time online calibration of magnetometer errors
  • ✔ Stable performance in dynamic and complex environments
  • ✔ Reliable output of angular velocity, acceleration, heading, and attitude data
  • ✔ High stability and strong anti-interference capability

🚀 Product Applications

This system is widely used in multiple industries and applications:

  • UAV navigation and flight control
  • Autonomous vehicle navigation
  • Marine navigation systems
  • Robotics control and positioning
  • Industrial automation equipment
  • Antenna stabilization systems
  • Surveying and mapping equipment
  • Precision orientation and positioning systems

Application Direction:

  • Navigation
  • Control
  • Measurement
  • Positioning & Orientation

⭐ Why Choose Us

  • Proprietary algorithm with independent intellectual property
  • High-precision MEMS technology
  • Strong anti-interference capability
  • Reliable performance in dynamic environments
  • Industry-grade stability and accuracy
  • Flexible integration with various systems
  • Professional technical support and customization services

We are committed to providing high-precision, reliable inertial navigation solutions for professional applications.


❓ Frequently Asked Questions (FAQ)

Q1: What type of sensors are used in this system?
The system uses a high-precision MEMS Inertial Measurement Unit (IMU).

Q2: Does the system support dynamic environments?
Yes, it provides stable and reliable data output even in dynamic environments.

Q3: Can the magnetometer be calibrated automatically?
Yes, the system supports real-time online calibration using a magnetometer error ellipsoid model.

Q4: What data outputs are supported?
The system outputs angular velocity, acceleration, heading, and attitude data.

Q5: What applications is this product suitable for?
It is suitable for navigation, control, measurement, positioning, and orientation applications.

Parameter  unit fundamental form
курс angle accuracy (uniform magnetic field, RMS) ° 1.0
Roll angle accuracy / Yaw angle accuracy (RMS) ° Static: 0.1
° Dynamic: 0.2
 

 

 

 

 

gyroscope

measuring range ° /s ±480
Zero offset stability (10-second smoothing, 1σ, room temperature) ° /h 3
Full-temperature zero-drift variation (10-second smoothing, RMS, variable temperature) ° /h 20
Zero bias repeatability ° /h 5
random walk ° /  √ h 0.15
tape width Hz 250
Nonlinear scaling factor ppm 100
Scale factor repeatability ppm 100
cross coupling % 0.1
 

 

 

accelerometer

measuring range g ±20
Zero offset stability (10-second smoothing, 1σ, room temperature) mg 0.25
Full-temperature zero-drift variation (10-second smoothing, RMS, variable temperature) mg 3
Zero bias repeatability mg 0.5
tape width Hz 250
Scale factor repeatability ppm 500
cross coupling % 0.2
magnetometer measuring range guass ±2.5
sensitivity mguass/LSB 0.1
barometer pressure limit mbar 300~1100
sensitivity mbar/LSB 6.1*10-7
Data update rate Hz 200 (customizable)
voltage V 3.3±0.33
power dissipation W ≤ 0.5
working temperature ℃ -45~80
size mm 44*47*14
weight g 48±2
Interface —— TTL

China Moneypro KT-EX9-3-A MEMS Attitude and Heading Reference System (AHRS) Module

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CONTACT US

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    +86-18126437260
  • sales@moneyprouav.com
    moneyprouav@gmail.com
  • Office: East of the 16F, Building B, TCL Industrial Research Institute Building, No. 006, High-tech South Road, Nanshan District, Shenzhen City, China.
    Factory I: Building B , Gualan High-Technology Park, Longhua District, Shenzhen City, Guangdong Province.
    Factory II: Bajia Intelligent Equipment Garden, Boluo, Huizhou, Guangdong Province.
    Factory III: No. 169, Yingshanhong Road, Huangdao District, Qingdao City, Shandong Province.
  • What's App: +1-(213) 613-5938
    Telegram: +1-(213) 613-5938
    Wechat: +86-18126437260    
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