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Compact High Precision 9-Axis MEMS IMU with RS422

Compact High Precision 9-Axis MEMS IMU with RS422

MEMS Inertial Sense Imu

MEMS Micro Inertial Measurement Unit

Autonomous Inertial Sense Imu

Place of Origin:

China

Brand Name:

Liocrebif

Certification:

GJB 9001C-2017

Model Number:

LKF-MSU204A

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Product Details
Dimensions:
4.7*4.4*1.4cm
Color&Classification:
LKF-MSU204A
Brand:
Liocrebif
Output Format:
RS422
Application:
Anti-vibration And Attitude Control Of Industrial Equipment, Automatic Control, Robot Control, Pan-tilt L Stabilization And Control, Instrumentation
Original Place:
China
Highlight:

MEMS Inertial Sense Imu

,

MEMS Micro Inertial Measurement Unit

,

Autonomous Inertial Sense Imu

Payment & Shipping Terms
Minimum Order Quantity
1
Price
5000-25000CHY
Packaging Details
Wooden box/Cardboard box/Container
Delivery Time
2-4 weeks
Payment Terms
T/T
Supply Ability
10000
Product Description
MEMS Inertial Measurement Unit

MOQ: 1
Size: L(4.7) * W(4.4) * H(1.4) cm
Specification Number: LKF-MSU204A

The LKF-MSU204A MEMS is a compact, high-precision 9-axis inertial measurement unit (IMU), designed for high-precision navigation, control and dynamic measurement of carriers. This inertial measurement module integrates MEMS gyroscopes, MEMS accelerometers and MEMS magnetometers within a single housing. Adopting highly reliable MEMS sensors, it can accurately measure angular rate, acceleration and magnetic field information of moving carriers under harsh environments, making it a general-purpose device for industrial applications.

The LKF-MSU204A inertial measurement module adopts an aluminum alloy housing, which is lightweight with high structural strength and excellent anti-vibration & anti-shock performance.

Technical Specifications
.

Gyroscope

Measurement Range


500


+500

°/s

Full-temperature Bias



100

300

°/h

Bias Stability

10s smoothing


5


°/h

Bias Instability

Allan variance


1


°/h

Bias Repeatability

Constant temperature


1.5

5

°/h

Angular Random Walk



0.1


°/√h

Scale Factor Non-linearity



25

100

ppm

Cross-coupling Error




0.001

Rad

Bandwidth


200



Hz

Accelerometer

Measurement Range


-16


+16

g

Full-temperature Bias



1

3

mg

Bias Stability

10s smoothing


0.03

0.1

mg

Bias Instability

Allan variance


0.01

0.03

mg

Bias Repeatability

Constant temperature


0.03

0.1

mg

Velocity Random Walk



0.01

0.03

m/s/√h

Scale Factor Non-linearity

±1 g input


100

200

ppm

Cross-coupling Error




0.001

Rad

Bandwidth


200



Hz

Magnetometer

Measurement Range


-8


+8

Gs

Resolution



200


μGs

Noise Density



50


μGs

Bandwidth



200


Hz

Barometer

Measurement Range


300


1100

mbar

Total Error



4.5


mbar

Absolute Error



1.5


mbar

Non-linearity



0.1


%FS

Resolution



0.1


mbar

Reliability

MTBF (Mean Time Between Failures)


20000



h

Continuous Operating Duration


120



h

Note: Typical values represent 1σ statistical results of multiple sample tests.

Main Features
  • 3-axis digital gyroscope, measurement range ±500 °/s
  • 3-axis digital accelerometer, measurement range ±16 g
  • Digital barometric pressure sensor, range 300 mbar ~ 1100 mbar
  • Full-temperature calibration and compensation from -40 ℃ to +80 ℃ (for gyroscopes and accelerometers)
  • SPI serial communication compatible
  • Built-in temperature sensor
  • Compact size and lightweight
  • Pin-to-pin compatible with ADIS16488A
Applications
  • Vibration suppression and attitude control of industrial equipment
  • Automatic control systems
  • Robot control
  • Gimbal stabilization and control
  • Instruments and meters
Dimensions
LKF-MSU204A MEMS Inertial Measurement Unit dimensional diagram showing physical size and layout
Figure 1: Dimension Diagram
Pin Definition
LKF-MSU204A MEMS Inertial Measurement Unit pin definition diagram showing connector pin assignments
Figure 2: Pin Definition Diagram
Additional technical diagram of LKF-MSU204A MEMS Inertial Measurement Unit
Figure 3: Technical Diagram

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