U6300 Mems High Precision Digital Output Imu Sensor 6-Axis Tactical-Grade Inertial Measurement Unit for Navigation & Robotics

Product Details
Customization: Available
Type: Gyroscope
Interface: RS422
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  • U6300 Mems High Precision Digital Output Imu Sensor 6-Axis Tactical-Grade Inertial Measurement Unit for Navigation & Robotics
  • U6300 Mems High Precision Digital Output Imu Sensor 6-Axis Tactical-Grade Inertial Measurement Unit for Navigation & Robotics
  • U6300 Mems High Precision Digital Output Imu Sensor 6-Axis Tactical-Grade Inertial Measurement Unit for Navigation & Robotics
  • U6300 Mems High Precision Digital Output Imu Sensor 6-Axis Tactical-Grade Inertial Measurement Unit for Navigation & Robotics
  • U6300 Mems High Precision Digital Output Imu Sensor 6-Axis Tactical-Grade Inertial Measurement Unit for Navigation & Robotics
  • U6300 Mems High Precision Digital Output Imu Sensor 6-Axis Tactical-Grade Inertial Measurement Unit for Navigation & Robotics
Find Similar Products
  • Overview
  • Specification
  • More similar products
  • Company Profile
  • FAQ
Overview

Basic Info.

Model NO.
U6300
Bandwidth
268
Weight
50g
Voltage
5
Vibration
6.06g (20-2000Hz)
Transport Package
Box and Sponge
Specification
47*44*14
Trademark
ML
Origin
China
HS Code
9031809090
Production Capacity
1000/Month

Packaging & Delivery

Package Size
50.00cm * 40.00cm * 40.00cm
Package Gross Weight
30.000kg

Product Description

Specification
Index item
U6300-A
U6300-B
U6300-C
U6300-D
Unit
Gyro
Measuring Range: X, Y, Z
±450
°/s
Bias instability
0.5
0.3
0.2
0.1
°/h
Random walk
0.02
º/√hr
Zero bias stability
1
°/h
Full-temperature bias stability
5
°/h
Non-Linearity
100
ppm
Orthogonality
100
ppm
Bandwidth
268
Hz
Accl
Measuring Range: X, Y, Z
±20
g
Bias instability
10
μg
Random walk
0.02
m/s/√hr
Zero bias stability
100
μg
Full-temperature bias stability
<150
μg
Non-Linearity
100
ppm
Orthogonality
100
ppm
Bandwidth
268
Hz
Basic parameters
Size
38.6*44.8*10
mm
Weight
50
g
Voltage
5
VDC
Power consumption
0.5
W
Interface
RS422

Output frequency
1000
Hz
Working Temperature
-40 ~ +85
°C
Storage Temperature
-55 ~ +105
°C
Vibration
6.06g (20-2000Hz)

Shocking
1500g / 0.5ms

More similar products
U6300 Mems High Precision Digital Output Imu Sensor 6-Axis Tactical-Grade Inertial Measurement Unit for Navigation &amp; Robotics
U6300 Mems High Precision Digital Output Imu Sensor 6-Axis Tactical-Grade Inertial Measurement Unit for Navigation &amp; Robotics
Company Profile
Micro Magic Company
Our inertial sensors are known for their high precision, long life and reliability, and are widely used in a variety of industries such as aerospace, automobiles, robotics, and consumer electronics. Strict production and factory inspection processes ensure that each sensor can meet the high requirements of the industry. We provide customized solutions to meet customer-specific needs and help technological innovation in various industries.
U6300 Mems High Precision Digital Output Imu Sensor 6-Axis Tactical-Grade Inertial Measurement Unit for Navigation &amp; Robotics
U6300 Mems High Precision Digital Output Imu Sensor 6-Axis Tactical-Grade Inertial Measurement Unit for Navigation &amp; Robotics
U6300 Mems High Precision Digital Output Imu Sensor 6-Axis Tactical-Grade Inertial Measurement Unit for Navigation &amp; Robotics
FAQ
Q1: What is the U6300 IMU?
A: The U6300 is a high precision MEMS Inertial Measurement Unit (IMU). It integrates a 3-axis gyroscope and a 3-axis accelerometer, supporting output of angular velocity, acceleration, and attitude angles.

Q2: What are the main features?
A:Gyroscope range: ±450 °/s
Accelerometer range: ±20 g
Bandwidth: 268 Hz
RS422 digital communication interface
Compact size: 38.6 × 44.8 × 10 mm, weight 50 g
Operating temperature: –40 °C ~ +85 °C
Output frequency up to 1000 Hz.
Q3: What applications is it suitable for?
A: Autonomous driving and intelligent transportation
Civilian and special-purpose drones (UAVs)
Automated machinery and AGVs
Robotics control
Railway positioning and communication platforms
Personnel navigation and platform stability

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