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Integrated MEMS Inertial Unit Long Term DC 5V For Flight Control

Integrated MEMS Inertial Unit Long Term DC 5V For Flight Control

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
Essential details
MOQ:1
Size:L(2.24)*W(2.25)*H(9) cm
Specification Number:LKF-MSU102
Product Introduction

Technical Characteristics

Customizable precision and wide range of applications

The LKF-MSU102 MEMS Inertial Measurement Unit is a compact, high-precision, high-reliability, and cost-effective three-axis MEMS inertial module capable of measuring the three-dimensional angular velocity and acceleration of a moving carrier. The module performs full-temperature compensation for parameters including bias, scale factor, non-orthogonality, and acceleration-related errors, ensuring long-term measurement accuracy.

 

Advanced processes and technologies

The LKF-MSU102 MEMS inertial unit integrates high-performance MEMS gyroscopes and MEMS accelerometers within an independent structure. The gyroscopes and accelerometers used in this unit represent the cutting edge of MEMS inertial device technology. The tri-axis MEMS gyroscopes are sensitive to angular motion of the carrier, while the tri-axis MEMS accelerometers capture linear acceleration. Internal compensation is applied across the full temperature range for bias, scale factor, non-orthogonality, and acceleration-related terms, ensuring sustained high accuracy. Additionally, the unit features a sealed design to maintain precise measurements of angular and linear motion even under harsh environmental conditions, offering users a cost-effective and highly reliable solution.

 

Table 1 Performance Parameters Of LKF-MSU102

MEMS Gyroscope

Note

Range

-500°/s~+500°/s

 

Bias over full temperature range

0.15°/s

 

Bias stability

15°/h

10s smoothing

Bias instability

5°/h

Allan

Bias repeatability

15°/h

 

Angular Random Walk

0.5°√h

 

Scale factor nonlinearity

100ppm

 

Adjustable bandwidth

100Hz

 

MEMS Accelerometer

 

Range

-20g~+20g

 

Bias

5mg

 

Bias stability

0.2mg

10s smoothing

Bias instability

0.05mg

Allan

Bias repeatability

0.2mg

 

Velocity Random Walk

0.05m/s/√h

 

Bias instability(Allan)

0.05mg

 

Scale factor nonlinearity ( ±1g)

300ppm

 

Scale factor nonlinearity ( ±1g)

200ppm

 

Adjustable bandwidth

100Hz

 

System

 

Power Supply

5V±0.2V

 

Operating Temperature

-40~+80

 

Shock

2000g

 

Vibration

6.06grms

20~2000Hz

Size

22.4mm×22.5mm×9mm

 

Weight

20g

 

Adjustable Data Update Rate

1000Hz

 

Interface Type

UART

LVTTL level

 

Table 2 MSU102 MEMS IMU Pin Definition

Wire Harness

No.

Color

Definition

Connector

No.

Wire Harness (Diameter0.07 mm)

1

Red

+5V

DB9_M1

6

2

Black

GND

5

3

Orange

UART_TX

1

4

Yellow

UART_RX

2

5

Blue

PPS

3

6

White

TOV

4

 

 

 

 

 

 

 

 

 

Main features

Full temperature compensation

Excellent temperature performance

Data update rate up to 1000 Hz

Configurable baud rate, up to 921.6 kbps

Powered by DC 5V

Supports software online upgrade

 

Applications

Flight control

Autonomous driving

Attitude reference

Mobile mapping

 

Fig. 1 Outline Structure Dimension Diagram

Integrated MEMS Inertial Unit Long Term DC 5V For Flight Control 0

 
 
Integrated MEMS Inertial Unit Long Term DC 5V For Flight Control 1
 

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