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Home » Unmanned System Products » China Moneypro KT-EX6-7-A MEMS Attitude and Heading Reference System (AHRS) Module
China Moneypro KT-EX7-1 North-Seeking Gyroscope (North Finder) Module
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China Moneypro KT-EX6-27-A MEMS Attitude and Heading Reference System (AHRS) Module

China Moneypro KT-EX6-7-A MEMS Attitude and Heading Reference System (AHRS) Module

This high-performance MEMS inertial measurement unit (IMU) is composed of MEMS gyroscope chips, MEMS accelerometer chips, structural components, and embedded software. It integrates advanced compensation algorithms including full-temperature calibration, installation misalignment compensation, and nonlinear error correction. The system delivers stable and reliable output of angular velocity, acceleration, and attitude data under static, dynamic, and harsh environmental conditions, making it ideal for 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 control systems, users often face several technical limitations:

  • Sensor drift and accuracy degradation under temperature variation
  • Installation misalignment affecting measurement precision
  • Poor stability in dynamic or high-vibration environments
  • Lack of reliable attitude data in harsh operating conditions
  • High dependency on external correction systems (e.g., GNSS/GPS)
  • Insufficient performance consistency across different working scenarios

These issues reduce system reliability in precision navigation, control, and measurement applications.


⚙ Product Advantages

This MEMS IMU is designed to overcome these challenges through advanced sensing and compensation technologies:

  • ✔ Integrated MEMS gyroscope and accelerometer chip architecture
  • ✔ Built-in full temperature compensation algorithm for stable output
  • ✔ Installation misalignment angle compensation for improved accuracy
  • ✔ Nonlinear error correction for enhanced measurement precision
  • ✔ Provides real-time angular velocity, acceleration, and attitude data
  • ✔ Stable performance in static, dynamic, and harsh environments
  • ✔ High reliability for long-term continuous operation

The system ensures consistent, high-precision inertial data output even under complex operational conditions.


🧭 Product Applications

This MEMS IMU is widely used in high-precision industrial and aerospace-related fields:

  • Navigation systems (GNSS/INS integrated navigation)
  • Flight control systems for UAVs and drones
  • Industrial motion control and robotics
  • Measurement and stabilization platforms
  • Positioning and orientation systems
  • Autonomous vehicle and intelligent transportation systems

⭐ Why Choose Us

  • Advanced MEMS sensing technology with high stability
  • Multi-layer compensation algorithms for real-world accuracy
  • Strong adaptability in harsh and dynamic environments
  • Reliable performance in long-term continuous operation
  • Suitable for both industrial and aerospace-grade applications
  • Optimized for integration into navigation and control systems

We provide stable, high-precision inertial data solutions for demanding applications requiring accuracy and reliability.


❓ Frequently Asked Questions (FAQ)

Q1: What data does this IMU output?
It outputs angular velocity, acceleration, and attitude information after compensation.

Q2: Does it work in high-temperature or low-temperature environments?
Yes, it includes full-temperature compensation for stable performance across wide temperature ranges.

Q3: Can it be used in dynamic motion conditions?
Yes, it is designed to maintain accuracy under both static and dynamic conditions.

Q4: Is it suitable for navigation systems?
Yes, it is widely used in inertial navigation and positioning systems.

Q5: Does it require external calibration?
No, it includes built-in compensation algorithms to reduce external calibration dependency.

Parameter  unit fundamental form
Course angle drift (initial value 0°, RMS) ° /h 72
Roll angle accuracy / Yaw angle accuracy (RMS) ° Static: 0.2
° Dynamic: 0.3
 

 

 

 

 

gyroscope

measuring range ° /s ±500
Zero offset stability (10-second smoothing, 1σ, room temperature) ° /h 10
Full-temperature zero-drift variation (10-second smoothing, RMS, variable temperature) ° /h 60
Zero bias repeatability ° /h 20
random walk ° /  √ h 0.5
tape width Hz 100
Nonlinear scaling factor ppm 200
Scale factor repeatability ppm 200
cross coupling % 0.2
 

 

 

 

accelerometer

measuring range g ±40
Zero offset stability (10-second smoothing, 1σ, room temperature) mg 0.2
Full-temperature zero-drift variation (10-second smoothing, RMS, variable temperature) mg 2
Zero bias repeatability mg 1
tape width Hz 100
Scale factor repeatability ppm 500
cross coupling % 0.1
Data update rate Hz 200 (customizable)
voltage V 5±0.25
power dissipation W ≤ 0.4
working temperature ℃ -45~80
size mm 22*20*10.2
weight g ≤ 12
Interface —— RS-422

China Moneypro KT-EX6-7-A MEMS Attitude and Heading Reference System (AHRS) Module

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  • 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.
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  • What's App: +1-(213) 613-5938
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