High Performance Imu Inertial Measurement Unit Module

Product Details
Customization: Available
Type: Inertial Measurement Unit
Output Signal Type: Digital Output
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Registered Capital
1000000 RMB
Plant Area
>2000 square meters
  • High Performance Imu Inertial Measurement Unit Module
  • High Performance Imu Inertial Measurement Unit Module
  • High Performance Imu Inertial Measurement Unit Module
  • High Performance Imu Inertial Measurement Unit Module
  • High Performance Imu Inertial Measurement Unit Module
  • High Performance Imu Inertial Measurement Unit Module
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Basic Info.

Model NO.
IMU488M
Measuring Shaft Quantities
10
Accuracy Grade
1degree/H
IP Rating
IP67
Certification
ISO
Customized
Non-Customized
Transport Package
Carton
Specification
47*44*14mm
Trademark
SkyMEMS
Origin
China
HS Code
9014100000
Production Capacity
2000/Month

Product Description

IMU488M High Performance Imu Inertial Measurement Unit Module

High Performance Imu Inertial Measurement Unit Module
Main Features
- Precision 10 DoF MEMS Inertial Measurement Unit

- Dynamic Range: Gyro ±450°/s,  Acc ±16g
- Bias Stability: Gyro: 1°/h, Acc 45µg (Allan)
- Full Temperature Range Accuracy: Built-in High
  Performance Temperature Calibration and
  Compensation Algorithm

High Performance Imu Inertial Measurement Unit Module
Brief Introduction
IMU488M
Inertial Measurement Unit is a high performance tactical grade MEMS Inertial Measurement Unit, it is composed of 1°/h (Allan) bias stability MEMS gyroscope and 45µg (Allan) bias stability MEMS accelerometer, which can output precise 3-axis outputs of angular rate, 3 axis acceleration data, 3 axis magnetometer data, and barometer data, etc.

IMU488M Inertial Measurement Unit adopts latest MEMS technology and advanced MEMS components, which reduces the cost deeply. The system enjoys small size and light weight, and it has been widely applied in tactical UAS Navigation & Control, Precise Guided Bomb, Rocket, Seeker, Platform Stabilization, etc.

High Performance Imu Inertial Measurement Unit Module
Technical Specifications 
Technical Specs
Parameter           Test Condition Value Unit
Min Typical Max
Gyroscopes
Dynamic Range   ±400 ±450 - °/s
Bias Stability Allan variance - 1.0 - °/h
Bias Repetition Bias range in full temperature range: -40~+85°C - 0.08 0.12 °/s
Scale Factor Scale factor  repetition, full temperature range: -40~+85°C - 150   ppm
Scale factor nonlinearity, FS=450°/s   150   ppm
Radom Walk     0.15   º/√h
Bandwidth       200 Hz
Accelerometer
Dynamic Range     ±16   g
Bias Stability Allan variance   0.015   mg
Radom Walk     0.025   m/s/√h
Bias Repetition full temperature range: -40~+85°C   1.0 2.0 mg
Scale Factor Repitition full temperature range: -40~+85°C   300   ppm
Scale factor nonlinearity     300   ppm
Bandwidth       200 Hz 3dB
Magnetometer
Dynamic Range     ±2   Gauss
Resolution     120   uGauss
Noise Density     50   uGauss
Bandwidth     200   Hz
Barometer
Pressure Range   450   1100 mbar
Resolution     0.1   mbar
Absolute Accuracy     1.5   mbar
Communication Interface
1 Channel SPI Baud rate     15 MHz
1 Channel UART Baud rate 115.2 460.8 921.6 Kbps
Sampling Rate SPI    2000   Hz
UART   200   Hz
 
Technical Specs
Parameter           Test Condition Value Unit
Min Typical Max
Electronic Characteristics
Voltage   4.5 5.0 5.5 V
Power Consumption       0.5 W
Ripple Wave P-P     100 mV
Physical Characteristics
Dimension     47*44*14   mm
Weight     50   grams
Working Environment
Working Temperature   -40   85 °C
Storage Temperature   -45   105 °C
Vibration Resistance     10~2000Hz, 3g    
Shock Resistance     30g, 11ms    
Overload Resistance half sine, 0.5ms   1000   g
Reliability
MTBF     20000   h
Continuous Working Time     120   h


High Performance Imu Inertial Measurement Unit Module
Typical Applications
-Tactical UAS Navigation & Control
- Unmanned Vehicle
- Platform Stabilization


High Performance Imu Inertial Measurement Unit Module

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