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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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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

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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

1836V(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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