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High Accuracy Compact Size Low Power Consumption Inertial Measurement Unit (IMU) for Aerospace and Robotics
High Accuracy Compact Size Low Power Consumption Inertial Measurement Unit (IMU) for Aerospace and Robotics
High Accuracy Compact Size Low Power Consumption Inertial Measurement Unit (IMU) for Aerospace and Robotics
High Accuracy Compact Size Low Power Consumption Inertial Measurement Unit (IMU) for Aerospace and Robotics
Specifications
Brand Name :
The Inertial Measurement Unit (IMU)
Model Number :
F41IMU
Certification :
CCS
Place of Origin :
China
MOQ :
one set
Payment Terms :
T/T
Supply Ability :
30 set per month
Delivery Time :
15 Days
Packaging Details :
carton box
Ground tracking inaccuracy :
Ship's speed (less than 1 kn)： ±0.01 m/s, whichever is greater Ship's speed (more than 1 kn)： ±1.0 % or ±0.1 kn, whichever is greater
Water tracking inaccuracy :
±1.0 % or ±0.1 kn, whichever is greater
Depth range :
1-200 m
Transducer diameter :
Ø112
Gate Valve diameter :
Ø125
Gate Valve weight :
120 kg
Input Range :
400°/s
Interface :
I2C, SPI, UART
Dimensions :
Varies by model, typically in mm scale
Applications :
Aerospace, Robotics, Smartphones, Drones, Automotive
Operating Temperature Range :
-40°C to +85°C
Components :
Accelerometer, Gyroscope, Magnetometer
Random Walk Coefficient :
0.02°/√h
Type :
Sensor
Degrees of Freedom :
6-DOF or 9-DOF
Calibration :
Factory calibrated or user calibratable
Zero Bias Repeatability :
0.005°/h
Output :
Digital or Analog Signals
Output Data Format :
Quaternion, Euler Angles, Raw Sensor Data
Measurement :
Acceleration, Angular Velocity, Magnetic Field
Weight :
Typically less than 50 grams
Description

The Inertial Measurement Unit (IMU) features advantages such as compact size, light weight, low power consumption, and high precision. It can be used to design pure strapdown, single-axis, and dual-axis modulated inertial navigation systems, meeting the demand for small-size, high-precision inertial navigation equipment in new unmanned platforms, underwater/torpedo weaponry, as well as land-based and airborne weapon platforms. It possesses the capability for dynamic measurement of carrier angular and linear motion information.

Technical Parameters


Item

Indicator

Description

Parameter

Remark

Gyro

Zero Bias

Bias Stability (10s)

0.3°/h

Zero Bias Stability at Variable Temperature (100s)

0.5°/h

Scaling Factor

Scale Factor Nonlinearity

≤20ppm

Other Indicators

Random Walk Coefficient

0.02°/½h

Input Range

400°/s

Accelerometer

Deviation

Zero Bias Repeatability

0.3mg

Zero Bias

Bias Temperature Sensitivity

50μg/℃

Scaling Factor

Scale Factor Repeatability

300ppm

Scale Factor Temperature Sensitivity

20ppm/℃

Range Indicators

Input Range

±20g

Characteristics

Environmental Performance

Operating Temperature

-40℃～60℃

Storage Temperature

-45℃～70℃

General Requirements

Power Supply

18～36V(DC)

Stable Power Consumption

≤8W

Startup Power Consumption ≤15W

Mounting Hole Diameter

4-Φ4.5mm

Dimensions(mm)

70.3×70.3×53

Weight

≤500g

Structure Diagram

High Accuracy Compact Size Low Power Consumption Inertial Measurement Unit (IMU) for Aerospace and Robotics


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High Accuracy Compact Size Low Power Consumption Inertial Measurement Unit (IMU) for Aerospace and Robotics

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Product Detail
Brand Name :
The Inertial Measurement Unit (IMU)
Model Number :
F41IMU
Certification :
CCS
Place of Origin :
China
MOQ :
one set
Payment Terms :
T/T
Contact Supplier
High Accuracy Compact Size Low Power Consumption Inertial Measurement Unit (IMU) for Aerospace and Robotics
High Accuracy Compact Size Low Power Consumption Inertial Measurement Unit (IMU) for Aerospace and Robotics

QINGDAO NAVI OPTICS TECHNOLOGY CO.,LTD

Verified Supplier
7 Years
qingdao
Since 2014
Business Type :
Manufacturer, Distributor/Wholesaler, Agent, Importer, Exporter
Main Products :
Inertial Navigation System, Fiber Optic Gyrocompass, Fiber Optic Gyroscope
Total Annual :
4,800,000-5,200,000
Employee Number :
100~120
Certification Level :
Verified Supplier
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