Home > Products > MEMS IMU >
High Reliability RS422 Output MEMS Inertial Measurement Unit with Compact Size for UAV and Vehicle Applications

High Reliability RS422 Output MEMS Inertial Measurement Unit with Compact Size for UAV and Vehicle Applications

MEMS Inertial Measurement Unit Imu Sensor

MEMS Inertial Management Unit

Reliable Inertial Management Unit

Place of Origin:

China

Brand Name:

Liocrebif

Certification:

GJB 9001C-2017

Model Number:

LKF-MSU203

Chat Now
Request A Quote
Product Details
Dimensions:
4.48*3.86*2.15cm
Color&Classification:
LKF-MSU203
Brand:
Liocrebif
Output Format:
RS422
Application:
Radar/infrared Antenna Stabilization Platforms, UAV Attitude Reference/flight Path Control, Missile Flight Control Vehicle/ship Attitude Measurement, Port Measurement Systems, Satellite Communication On-the-move, Drilling And Extraction Systems, Mobile Ma
Original Place:
China
Highlight:

MEMS Inertial Measurement Unit Imu Sensor

,

MEMS Inertial Management Unit

,

Reliable Inertial Management Unit

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(4.48) × W(3.86) × H(2.15) cm

Specification Number: LKF-MSU203

Product Introduction
The LKF-MSU203 MEMS inertial measurement module is a high-reliability, cost-effective six-axis MEMS inertial measurement unit (IMU). It is widely applied in navigation, control and measurement fields represented by vehicles, ships and UAVs. The whole system adopts fully domestically manufactured electronic components. The built-in gyroscopes and accelerometers adopt state-of-the-art domestically produced MEMS inertial sensor technology. Customized hardware and software configurations are available for the LKF-MSU203 series inertial measurement modules to satisfy diverse user demands.
Performance Parameters
Parameter Technical Index
Gyroscope
Measurement Range (°/s) ±500
Full-Temperature Bias (°/h, 3σ) ≤30
Bias Stability (°/h, 10s averaging window) ≤2
Bias Instability (°/h, Allan variance, typical) ≤0.1
Bias Repeatability (°/h) ≤1
Angular Random Walk (°/√h) ≤0.1
Scale Factor Nonlinearity (ppm) ≤100
Cross-Coupling Error (rad) ≤0.001
Bandwidth (Hz) ≥200 Hz
Accelerometer
Measurement Range (g) ±30
Full-Temperature Bias (mg, 3σ) ≤2
Bias Stability (μg, 10s averaging window) ≤50
Bias Instability (μg, Allan variance, typical) ≤30
Bias Repeatability (μg) ≤50
Velocity Random Walk (m/s/√h) ≤0.03
Scale Factor Nonlinearity (ppm, ±1g input) ≤100
Cross-Coupling Error (rad) ≤0.001
Bandwidth (Hz) ≥200 Hz
Physical Characteristics
Supply Voltage (V) 5~12 (ripple ≤100 mV)
Steady-State Power Consumption (W) ≤2
Startup Time (s) ≤2
Maximum Data Update Rate (Hz) 2000
Overall Dimension (mm×mm×mm) 44.8×38.6×21.5
Weight (g) 52±5
Operating Environment
Operating Temperature (℃) -40 ~ 80
Storage Temperature (℃) -55 ~ 85
Vibration (g, RMS, 20~2000 Hz) 6.06
Shock (g, 1 ms half-sine pulse) 500
Connector Pin Definitions
Pin No. Definition Remarks
8 POWER_IN Power supply range: 5 V ~ 12 V (output ripple ≤ 100 mV)
15 GND
6 RS232_TXD1 RS232 communication interface
5 RS232_RXD1
3 GND
10 RS422 R+ M1: RS422 communication interface
2 RS422 R-
9 RS422 T+
1 RS422 T-
14 RS232_TXD2 M2: RS232 communication interface, supports external GNSS module input for timestamp tagging
7 RS232_RXD2
13 GND
11 PPS_IN
4 TOV General-purpose IO port, 3.3 V logic level, rising edge active
12 GND
Main Features
  • 100% domestically manufactured components
  • High performance, compact size, light weight and low power consumption
  • Full-temperature calibration and compensation from -40℃ to +80℃
  • High-speed sampling capability
  • Excellent resistance to harsh mechanical environments
  • Support for on-board software upgrade
  • Pin-to-pin replacement for STIM300
Applications
  • Antenna stabilization platforms
  • UAV attitude reference & trajectory control
  • Flight control systems
  • Vehicle and ship attitude measurement
  • Port measurement systems
  • Mobile satellite communication terminals
  • Mobile mapping systems
  • Automated driving test systems
  • Personal navigation systems
Dimensions
LKF-MSU203 MEMS Inertial Measurement Unit dimensional diagram LKF-MSU203 MEMS Inertial Measurement Unit dimensional specifications

Send your inquiry directly to us

Privacy Policy China Good Quality Fiber Optic Gyroscope Supplier. Copyright © 2025-2026 Wuhan Liocrebif Technology Co., Ltd . All Rights Reserved.