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LKF-MNU107 MEMS Inertial Measurement Unit with High-speed sampling 1kHz, Full-temperature calibration -40°C to +80°C, and Resistance to harsh mechanical environments

LKF-MNU107 MEMS Inertial Measurement Unit with High-speed sampling 1kHz, Full-temperature calibration -40°C to +80°C, and Resistance to harsh mechanical environments

RS422 Mems Imu Sensor

RS422 IMU Inertial Measurement Unit

High Accuracy Mems Imu Sensor

Place of Origin:

China

Brand Name:

Liocrebif

Certification:

GJB 9001C-2017

Model Number:

LKF-MNU107

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Product Details
Output Format:
RS422
Dimensions:
5.5*5.5*1.5 Cm
Power Supply:
5±0.2 V
Power:
≤1 W
Startup Time:
≤2 S
Update Rate:
1000 Hz
Highlight:

RS422 Mems Imu Sensor

,

RS422 IMU Inertial Measurement Unit

,

High Accuracy Mems Imu Sensor

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
LKF-MNU107 MEMS Inertial Measurement Unit
Product Overview

The LKF-MNU107 is a highly reliable and cost-effective three-axis MEMS inertial sensor designed for navigation, control, and measurement applications, particularly in inertial navigation systems.

This unit integrates high-performance MEMS gyroscopes and MEMS accelerometers with comprehensive internal compensation for bias, scale factor, non-orthogonality errors, and acceleration-related terms across full temperature parameters, ensuring sustained high measurement accuracy over extended periods.

Manufactured using strict processes, the LKF-MNU107 guarantees exceptional reliability and consistent performance.

Key Features
  • Multi-sensor redundancy and fault-tolerant design
  • High performance with compact size and low power consumption
  • -40°C to +80°C full-temperature calibration and compensation
  • 1kHz high-speed sampling capability
  • Resistance to harsh mechanical environments
  • Software online upgrade capability
Applications
  • High-overload missile-borne applications
  • Flight control systems
Technical Specifications
MEMS Gyroscope
Range (°/s) X-axis: ±5400°/s, Y/Z-axis: ±500°/s
Bias @ Full temp. (°/s, 3σ) ≤360
Bias Stability (°/h, 10s smoothing) ≤20
Bias Repeatability (°/h) ≤20
Bias Instability (°/h, Allan, typ) ≤5
Angular Random Walk (°/√h) ≤0.8
Scale Factor Nonlinearity (ppm) ≤100
Cross-Coupling (rad) ≤0.001
Bandwidth (Hz) ≥200Hz
MEMS Accelerometer
Range (g) ±20
Bias @ Full temp. (mg, 3σ) ≤20
Bias Stability (μg, 10s smoothing) ≤500
Bias Instability (μg, Allan, typ) ≤100
Bias Repeatability (μg) ≤500
Velocity Random Walk (m/s/√h) ≤0.06
Scale Factor Nonlinearity (ppm, ±1g) ≤300
Cross-Coupling (rad) ≤0.001
Bandwidth (Hz) ≥200Hz
Electrical/Mechanical Interface
Power Supply (V) 5±0.2
Power (W) ≤1
Startup Time (s) ≤2
Communication interface RS-422
Update Rate (Hz) 1000
Dimensions (mm*mm*mm) Ф55 * 15
Weight (g) ≤60
Operating Environment
Operating Temp. (°C) -40~80
Storage Temp. (°C) -55~85
Vibration (g, Rms) 6.06, 20~2000Hz
Shock (g) 15000/10ms
LKF-MNU107 MEMS Inertial Measurement Unit product image

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