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


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

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Product Detail
MOQ :
1set
Interface :
SPI,UART
Model Number :
SI-MIMU-P
Technology :
Micro-Electro-Mechanical Systems (MEMS)
Bias stability :
≤10°/h
Delivery Time :
5-8 work days
Contact Supplier
SI‑MIMU‑P 10‑Axis MEMS IMU | ADIS16488 Pin-to-Pin Replacement for UAV Attitude Control

Stable Inertial Systems Ltd.

Verified Supplier
1 Years
beijing, beijing
Since 1997
Business Type :
Manufacturer, Seller
Main Products :
MEMS Inertial Measurement Unit, MEMS Inertial Navigation System, Single Axis Gyroscope
Total Annual :
5000000-10000000
Employee Number :
500~1000
Certification Level :
Verified Supplier
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