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High Performance RS422 MEMS IMU Sensor

High Performance RS422 MEMS IMU Sensor

Integrated MEMS Inertial Unit 

Integrated inertial measurement units imus

Long Term MEMS Inertial Unit 

Place of Origin:

China

Brand Name:

Liocrebif

Certification:

GJB 9001C-2017

Model Number:

LKF-MSU102

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Product Details
Dimensions:
2.24×2.25×9cm
Color&Classification:
LKF-MSU102
Brand:
Liocrebif
Output Format:
RS422
Application:
Guidance Weapons Operating In Harsh Mechanical/thermal Conditions, UAV/vehicle/ship/boat Attitude Reference, Attitude Control Systems, Radar/infrared Antenna Stabilization Platforms
Original Place:
China
Highlight:

Integrated MEMS Inertial Unit 

,

Integrated inertial measurement units imus

,

Long Term MEMS Inertial 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
Product Overview

MOQ: 1

Size: L(2.24) * W(2.25) * H(9) cm

Specification Number: LKF-MSU102

Technical Characteristics
Customizable Precision and Wide Range of Applications

The LKF-MSU102 MEMS Inertial Measurement Module is a high-reliability, cost-effective six-axis MEMS inertial measurement unit, widely applied in navigation, control and measurement fields represented by vehicles, ships and UAVs.

Custom hardware and software configurations of the LKF-MSU102 series inertial measurement modules are available to meet diverse user requirements.

Advanced Processes and Technologies

The LKF-MSU102 series inertial measurement module integrates high-performance MEMS gyroscopes and MEMS accelerometers within an independent structural housing. The gyroscopes and accelerometers adopted in the system represent the cutting-edge level of inertial devices based on MEMS manufacturing technology.

The three-axis MEMS gyroscope senses the angular motion of the carrier, while the three-axis MEMS accelerometer captures the linear acceleration of the carrier. Built-in full-temperature compensation is implemented for Bias, scale factor, non-orthogonality error and acceleration-dependent terms, enabling sustained high measurement accuracy over long-duration operation.

Performance Parameters

Parameter

Technical Index

Gyroscope

Measurement Range (°/s)

±500

Full-Temperature Bias (°/h, 3σ)

≤180

Bias Stability (°/h, 10s smoothing)

≤10

Bias Instability (°/h, Allan variance, typical)

≤2

Bias Repeatability (°/h)

≤10

Angular Random Walk (°/√h)

≤0.2

Scale Factor Nonlinearity (ppm)

≤100

Cross-Coupling Error (rad)

≤0.001

Bandwidth (Hz)

≥200 Hz

Accelerometer

Measurement Range (g)

±16

Full-Temperature Bias (mg, 3σ)

≤5

Bias Stability (μg, 10s smoothing)

≤300

Bias Instability (μg, Allan variance, typical)

≤40

Bias Repeatability (μg)

≤300

Velocity Random Walk (m/s/√h)

≤0.04

Scale Factor Nonlinearity (ppm, ±1g)

≤200

Cross-Coupling Error (rad)

≤0.001

Bandwidth (Hz)

≥200 Hz

Physical Characteristics

Maximum Output Update Rate (Hz)

1000

Dimension (mm×mm×mm)

22.4×23×9

Weight (g)

18±3

Operating Environment

Operating Temperature (℃)

-40 ~ 80

Storage Temperature (℃)

-55 ~ 85

Vibration (g, RMS)

20~2000 Hz, 6.06

Shock (g)

1000 / 1 ms


Pin Definition
Pin No. Definition Remarks
1 TOV Sampling Synchronization Pulse (LVTTL)
2 PPS_IN PPS Input (LVTTL)
3 UART_RX UART Receive (LVTTL)
4 UART_TX UART Transmit (LVTTL)
5 GND Power Ground
6 VCC (+5V) Positive Power Supply
Main Features
  • Multi-sensor redundancy and fault-tolerant design
  • High performance, compact size, light weight and low power consumption
  • Full-temperature calibration and compensation ranging from -40℃ to +80℃
  • High-speed sampling at 1 kHz
  • Resistance to harsh mechanical environments
  • Support for online software upgrade
Applications
  • Antenna stabilization platforms
  • UAV attitude reference & trajectory control
  • Flight control systems
  • Vehicle & ship attitude measurement
  • Port measurement systems
  • Mobile Satellite Communication (Mobile SATCOM)
  • Mobile mapping systems
  • Automated driving test systems
  • Personal navigation systems
Outline Structure Dimension Diagram
LKF-MSU102 MEMS Inertial Measurement Unit outline structure diagram view 1
LKF-MSU102 MEMS Inertial Measurement Unit outline structure diagram view 2
LKF-MSU102 MEMS Inertial Measurement Unit outline structure diagram view 3

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