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Home » Unmanned System Products » China Moneypro MOPKT-EX9-2 Nine-Degree-of-Freedom Inertial Measurement Unit Module
China Moneypro MOPKT-EX9-1 Six-Degree-of-Freedom Inertial Measurement Unit Module
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China Moneypro MOPKT-EX9-3 Nine-Degree-of-Freedom Inertial Measurement Unit Module

China Moneypro MOPKT-EX9-2 Nine-Degree-of-Freedom Inertial Measurement Unit Module

This high-performance inertial measurement unit (IMU) is composed of MEMS gyroscope chips, MEMS accelerometer chips, magnetometer chips, and barometric pressure sensors. It integrates advanced structural design and intelligent software algorithms, including full temperature compensation, installation misalignment compensation, and nonlinear error correction. The system delivers stable, reliable, and highly accurate measurement data under static, dynamic, and harsh environmental conditions. It is fully compatible with the ADIS16488 series, enabling seamless replacement and integration.

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

🚨 Industry Pain Points

In modern navigation, control, and measurement systems, users often face the following challenges:

  • Sensor drift and accumulated error in long-term operation
  • Performance degradation under extreme temperature conditions
  • Sensitivity to installation alignment and mechanical vibration
  • Inaccurate output in dynamic or high-maneuver environments
  • Lack of compatibility between different IMU systems
  • High cost of system integration and replacement upgrades

These issues significantly impact positioning accuracy, navigation stability, and system reliability.


⚙ Product Advantages

This IMU system is designed with advanced MEMS technology and intelligent compensation algorithms to solve the above problems:

  • ✔ Integrated MEMS gyroscope, accelerometer, magnetometer, and barometric pressure sensors
  • ✔ Built-in full temperature compensation for stable performance across wide temperature ranges
  • ✔ Installation misalignment compensation for improved mounting flexibility
  • ✔ Nonlinear error compensation algorithms for enhanced accuracy
  • ✔ Stable output under static, dynamic, and harsh environmental conditions
  • ✔ High compatibility with ADIS16488 series for direct replacement
  • ✔ Compact structure with high reliability and long service life

🎯 Product Applications

This IMU is widely used in precision industrial and aerospace systems, including:

  • Navigation systems (GNSS/INS integrated navigation)
  • Flight control systems for UAVs and aircraft
  • Motion control and stabilization platforms
  • High-precision positioning and orientation systems
  • Robotics and autonomous vehicle navigation
  • Surveying, mapping, and geospatial measurement

⭐ Why Choose Us

  • High-precision MEMS sensing technology with multi-sensor fusion
  • Advanced multi-layer error compensation algorithms
  • Strong adaptability for harsh environmental conditions
  • Drop-in compatibility with ADIS16488 series systems
  • Reliable performance for both static and dynamic applications
  • Designed for industrial-grade and aerospace-grade requirements

We provide stable, accurate, and integration-ready IMU solutions for demanding navigation and control applications.


❓ Frequently Asked Questions (FAQ)

Q1: Is this IMU compatible with ADIS16488?
Yes, it is designed to be fully compatible and can be used as a direct replacement.

Q2: Does it support harsh environmental conditions?
Yes, it maintains stable performance under static, dynamic, and harsh conditions.

Q3: What sensors are integrated in this product?
It includes MEMS gyroscope, accelerometer, magnetometer, and barometric pressure sensors.

Q4: Does it support temperature compensation?
Yes, it has full temperature compensation for improved measurement accuracy.

Q5: What are the main application areas?
It is used in navigation, control systems, measurement systems, and orientation positioning applications.

Parameter  unit fundamental form
gyroscope Measurement range (customizable) ° /s ±480
Zero-level offset ° /h 180
Zero-pitch instability (@ALLAN variance) ° /h 5
Zero offset stability (10-second smoothing, 1σ, room temperature) ° /h 10
Zero bias repeatability ° /h 20
Zero bias error across the entire temperature range ° /h 72
random walk ° /  √ h 0.26
Zero-zero acceleration sensitivity ° /h/g 20
resolution ratio ° /s 0.01
Output noise (half-maximum) ° /s 0.4
tape width Hz 330
Nonlinear scaling factor ppm 200
Scale factor repeatability ppm 200
cross coupling % 0.2

 

Parameter  unit fundamental form
accelerometer Measurement range (customizable) g ±20
Zero-pitch instability (@ALLAN variance) mg 0.07
Zero offset stability (10-second smoothing, 1σ, room temperature) mg 0.25
Zero bias repeatability mg 0.5
Zero bias error across the entire temperature range mg 3
random walk m/s/ √ h 0.029
resolution ratio mg 0.1
tape width Hz 250
Scale factor repeatability ppm 500
cross coupling % 0.2

 

Parameter  unit fundamental form
magnetometer Dynamic measurement range guass ±2.5
Sensitivity Value mguass/LSB 0.1
barometer pressure limit mbar 300~1100
sensitivity mbar/LSB 6.1*10 -7

 

Parameter unit fundamental form
 

 

 

other

Stabilization start time s 1
Data update rate Hz 2460
voltage V 3.3±0.15
steady state power consumption W 0.5
ripple wave mV 100
working temperature ℃ -45~85
storage temperature ℃ -55~85
weight g 48±2
size mm 44*47*14
Interface —— SPI

China Moneypro KT-EX9-2 Nine-Degree-of-Freedom Inertial Measurement Unit 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
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