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SI‑MIMU‑P 10‑Axis MEMS IMU | ADIS16488 Pin-to-Pin Replacement for UAV Attitude Control

SI‑MIMU‑P 10‑Axis MEMS IMU | ADIS16488 Pin-to-Pin Replacement for UAV Attitude Control

MOQ: 1set
Delivery Period: 5-8 work days
Payment Method: L/C,D/A,D/P,T/T,Western Union
Detail Information
Brand Name
SI
Model Number
SI-MIMU-P
Customized Support:
OEM, ODM
Technology:
Micro-Electro-Mechanical Systems (MEMS)
Interface:
SPI,UART
Power Supply Range:
5V DC
Applications:
Drones, Robotics, Automotive, Consumer Electronics, Navigation
Grade:
Industrial
Type:
Inertial Measurement Unit (IMU)
Bias Stability:
≤10°/h
Highlight:

10-axis MEMS IMU for UAV

,

ADIS16488 replacement IMU

,

MEMS inertial measurement unit with attitude control

Product Description

The TJ-MIMU-P Micro Inertial Measurement Unit (MIMU) is a professional inertial measurement device built on mature Micro-Electro-Mechanical System (MEMS) technology. It integrates a built-in three-axis MEMS gyroscope, three-axis MEMS accelerometer, three-axis magnetometer and barometric pressure sensor, matched with dedicated drive and signal acquisition circuits, temperature sensors, digital signal processing circuits, mechanical structures and supporting embedded software.

Adopting a proprietary structural design and equipped with comprehensive compensation algorithms covering full-temperature range, installation misalignment and nonlinearity, the MIMU delivers steady and reliable performance in static, dynamic and harsh working environments, providing high-stability measurement data for various application scenarios.

Product Features
  • High repeatability and operational reliability
  • Full-factor sensor compensation technology
  • Low vibration rectification error
  • Compact size, lightweight and low power consumption
  • Highly cost-effective structural and circuit design
Applications
  • Unmanned Aerial Vehicles
  • Autonomous Driving
  • Robotics
  • Surveying and Mapping

Main performance Parameters

Indicator Type Specification Unit
Gyroscope Range ±450 °/s
Bias stability(1б,10s Smooth) ≤10 °/h
Bias instability(Allan variance) ≤2 °/h
Bias Repeatability(1σ) ≤10 °/h
Angular random walk ≤0.25 °/√h
Scale Factor Repeatability ≤200 ppm
Scale Factor Nonlinearity ≤200 ppm
Bandwidth ≥330 Hz
Accelerometer Range ±16 g
Bias stability(1б,10s Smooth) ≤0.2 mg
Bias instability(Allan variance) ≤0.025 mg
Bias Repeatability(1σ) ≤0.2 mg
Angular random walk ≤0.025 m/s/√h
Scale Factor Repeatability ≤200 ppm
Scale Factor Nonlinearity ≥200 ppm
Bandwidth ≥330 Hz
Magnetic sensor Dynamic measurement range ±2.5 gauss
Resolution ≤0.12 mGauss
Noise Density ≤50 uGauss
Bandwidth ≥200 Hz
Barometer Pressure Range 450~1100 mbar
Resolution ≤0.1 mbar
Absolute Measurement Accuracy ≤1.5 mbar
Electrical properties Voltage 3~5.5 V
Power consumption ≤1.5 W
Others Weight ≤50 g
Size 47*44*14 mm
Interface SPI,UART -


SI‑MIMU‑P 10‑Axis MEMS IMU | ADIS16488 Pin-to-Pin Replacement for UAV Attitude Control


Products
PRODUCTS DETAILS
SI‑MIMU‑P 10‑Axis MEMS IMU | ADIS16488 Pin-to-Pin Replacement for UAV Attitude Control
MOQ: 1set
Delivery Period: 5-8 work days
Payment Method: L/C,D/A,D/P,T/T,Western Union
Detail Information
Brand Name
SI
Model Number
SI-MIMU-P
Customized Support:
OEM, ODM
Technology:
Micro-Electro-Mechanical Systems (MEMS)
Interface:
SPI,UART
Power Supply Range:
5V DC
Applications:
Drones, Robotics, Automotive, Consumer Electronics, Navigation
Grade:
Industrial
Type:
Inertial Measurement Unit (IMU)
Bias Stability:
≤10°/h
Minimum Order Quantity:
1set
Delivery Time:
5-8 work days
Payment Terms:
L/C,D/A,D/P,T/T,Western Union
Highlight

10-axis MEMS IMU for UAV

,

ADIS16488 replacement IMU

,

MEMS inertial measurement unit with attitude control

Product Description

The TJ-MIMU-P Micro Inertial Measurement Unit (MIMU) is a professional inertial measurement device built on mature Micro-Electro-Mechanical System (MEMS) technology. It integrates a built-in three-axis MEMS gyroscope, three-axis MEMS accelerometer, three-axis magnetometer and barometric pressure sensor, matched with dedicated drive and signal acquisition circuits, temperature sensors, digital signal processing circuits, mechanical structures and supporting embedded software.

Adopting a proprietary structural design and equipped with comprehensive compensation algorithms covering full-temperature range, installation misalignment and nonlinearity, the MIMU delivers steady and reliable performance in static, dynamic and harsh working environments, providing high-stability measurement data for various application scenarios.

Product Features
  • High repeatability and operational reliability
  • Full-factor sensor compensation technology
  • Low vibration rectification error
  • Compact size, lightweight and low power consumption
  • Highly cost-effective structural and circuit design
Applications
  • Unmanned Aerial Vehicles
  • Autonomous Driving
  • Robotics
  • Surveying and Mapping

Main performance Parameters

Indicator Type Specification Unit
Gyroscope Range ±450 °/s
Bias stability(1б,10s Smooth) ≤10 °/h
Bias instability(Allan variance) ≤2 °/h
Bias Repeatability(1σ) ≤10 °/h
Angular random walk ≤0.25 °/√h
Scale Factor Repeatability ≤200 ppm
Scale Factor Nonlinearity ≤200 ppm
Bandwidth ≥330 Hz
Accelerometer Range ±16 g
Bias stability(1б,10s Smooth) ≤0.2 mg
Bias instability(Allan variance) ≤0.025 mg
Bias Repeatability(1σ) ≤0.2 mg
Angular random walk ≤0.025 m/s/√h
Scale Factor Repeatability ≤200 ppm
Scale Factor Nonlinearity ≥200 ppm
Bandwidth ≥330 Hz
Magnetic sensor Dynamic measurement range ±2.5 gauss
Resolution ≤0.12 mGauss
Noise Density ≤50 uGauss
Bandwidth ≥200 Hz
Barometer Pressure Range 450~1100 mbar
Resolution ≤0.1 mbar
Absolute Measurement Accuracy ≤1.5 mbar
Electrical properties Voltage 3~5.5 V
Power consumption ≤1.5 W
Others Weight ≤50 g
Size 47*44*14 mm
Interface SPI,UART -


SI‑MIMU‑P 10‑Axis MEMS IMU | ADIS16488 Pin-to-Pin Replacement for UAV Attitude Control