• Three Axis Imu Accelerometer Gyro Fog Imu Inertial Measurement Unit
  • Three Axis Imu Accelerometer Gyro Fog Imu Inertial Measurement Unit
  • Three Axis Imu Accelerometer Gyro Fog Imu Inertial Measurement Unit
  • Three Axis Imu Accelerometer Gyro Fog Imu Inertial Measurement Unit

Three Axis Imu Accelerometer Gyro Fog Imu Inertial Measurement Unit

Output Signal Type: Digital Output
Measuring Shaft Quantities: Three
Accuracy Grade: 1.6deg
IP Rating: IP67
Certification: CE
Customized: Customized
Customization:
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  • Overview
  • Product Description
  • Main Functions
  • Product Display
  • Product Parameters
  • Electrical interface
  • Product Structure
  • Main Application Fields
  • Company Profile
Overview

Basic Info.

Model NO.
GI200A-A0
Gyro Range
± 500º/S
Gyro Zero Bias Stability
1.6º/H
Acc Range
± 200g
Accelerometer Zero Bias Stability
0.06mg (Allan)
Communication Interface
1 Route Uart, 1 Route Spi, 1 Routel Can
Power Consumption
≤1.5W
Mtbf
20000h
Angular Random Walk
0.3°/√hr
Vibration
20~2000Hz
Weight
50g
Transport Package
Sponge and Box
Specification
47mm*44mm*14mm
Trademark
AVIC
Origin
China
Production Capacity
500/Month

Product Description

Three Axis Imu Accelerometer Gyro Fog Imu Inertial Measurement Unit 

Product Description

  The GI200A-A0 (B0) -IMU is an inertial measurement unit (IMU) based on micromachining technology (MEMS), with built-in high-performance MEMS gyroscope and MEMS accelerometer, outputting 3 angular velocities and 3 accelerations.
 
  GI200A-A0 (B0) -IMU features high reliability and strong environmental adaptability. By matching different software, the product can be widely used in tactical and industrial UAV, intelligent ammunition, seeker, mobile communication, mapping and other fields.

Main Functions

  1. Three-axis digital gyroscope:
    1. ± 2000º/s dynamic measurement range;
    2. A0 bias stability: 6 °/h (GJB, 10s, Z-axis), 9 °/hH (GJB, 1s, Z-axis), 1.6 °/h (ALLAN, Z-axis);
    3. B0 bias stability: 3 °/h (GJB, 10s, Z-axis), 4.5 °/h (GJB, 1s, Z-axis), 0.8 °/h (ALLAN, Z-axis);
  2. Triaxial digital accelerometer:
    1. ± 200g dynamic measuring range;
    2. A0 bias stability: 0.4mg (GJB, 10s), 0.6mg (GJB, 1s), 0.06 mg (ALLAN);
    3. B0 bias stability: 0.2mg (GJB, 10s), 0.3mg (GJB, 1s), 0.03mg (ALLAN);
  3. Triaxial digital magnetometer: 2.5gauss
  4. Digital barometer: 300mbar ~ 1100mbar
  5. High reliability: MTBF > 20000h;
  6. Guaranteed accuracy within the full temperature range (-40 ºC ~ + 80 ºC): built-in high-performance temperature calibration and compensation algorithm;
  7. Suitable for operation under strong vibration (6.06 g, 20 ~ 2000 Hz);
  8. Suitable for working under high impact conditions (1000 g, 0.5ms);
  9. Interface: 1-route UART, 1-route SPI, 1-routeCAN.

Product Display

Three Axis Imu Accelerometer Gyro Fog Imu Inertial Measurement Unit
Three Axis Imu Accelerometer Gyro Fog Imu Inertial Measurement Unit

 

Product Parameters

Parameter Test conditions Minimum value Typical value Maximum value Unit
Gyro Dynamic measuring range     500 2000 º/s
Zero bias stability Allan variance, Z-axis   1.6   º/h
Allan variance, X and Y axis   3.2   º/h
10 s average (-40 ºC ~ + 80 ºC, constant temperature), Z-axis   6   º/h
1s average (-40 ºC ~ + 80 ºC, constant temperature), Z-axis   9   º/h
10 s average (-40 ºC ~ + 80 ºC, constant temperature), X axis and Y axis   12   º/h
1 s average (-40 ºC ~ + 80 ºC, constant temperature), X axis and Y axis   18   º/h
Zero bias Zero-bias range, Z-axis   ±0.14   º/s
Zero-bias range, X-axis and Y-axis   ±0.4   º/s
Zero bias change over full temperature range, Z-axis1   ±0.04   º/s
Zero bias change over full temperature range, X and Y axis1   ±0.12   º/s
Sequential start repeatability, Z-axis   0.004   º/s
Sequential start repeatability, X-Axis and Y-Axis   0.012   º/s
Daily start repeatability, Z-axis   0.006   º/s
Daily start repeatability,, X axis and Y axis   0.018   º/s
Effect of linear acceleration on bias   0.004   º/s/g
Influence of vibration on zero bias, change before and after vibration2   0.004   º/s/g
Influence of vibration on zero bias, change before and during vibration2   0.004   º/s/g
Scale factor Scale factor accuracy, Z-axis   0.6   %
Scale Factor Accuracy, X and Y Axis   1.2   %
Scale factor nonlinearity, Z-axis   0.02   %FS
Scale Factor Nonlinearity, X and Y Axis   0.04   %FS
Angular random walk     0.3   °/√hr
Noise density     0.002   °/s/√Hz
Resolution     3.052×107   º/s/LSB
Bandwidth     200   Hz
Accelerometer Dynamic measuring range     16 200 g
Zero bias stability Allan variance   0.06   mg
10 s average (-40 ºC ~ + 80 ºC, constant temperature)   0.4   mg
1s average (-40 ºC ~ + 80 ºC, constant temperature)   0.6   mg
Zero bias Zero bias range   16 30 mg
Zero bias change in full temperature range, peak-to-peak value1   10 20 mg
Sequential start repeatability   1.0   mg
Daily start repeatability   1.6   mg
Zero-bias temperature coefficient   0.1 0.2 mg/ºC
Scale factor Scale factor accuracy   4   %
Scale factor nonlinearity   0.2   %FS
Speed random walk     0.058   m/s/√hr
Noise density     0.05   mg/√Hz
Resolution     1.221×108   g/LSB
Bandwidth     200   Hz
Magnetometer Magnetic field range Brg,xy   ±1300   μT
Brg,z   ±2500   μT
Resolution     0.3   μT
Heading and longitude 30 μT horizontal geomagnetic component, 25 ºC   ±2.5   deg
Dynamic measuring range     2.5   gauss
Zero bias Non-magnetic environment   15   mgauss
Barometer Dynamic measuring range   300   1100 mbar
Zero bias     4.5   mbar
Communication interface 1-route SPI Baud rate     15 MHz
1-route UART Baud rate   230.4   Kbps
1-route CAN Baud rate     1 MHz
Sampling frequency SPI   200 1000 Hz
UART   200   Hz
CAN   200    
Electrical characteristics Voltage   3.0 3.3 3.6 V
Power consumption       1.5 W
Ripple P-P     100 mV
Settling time From 0 V to 3.3 V     80 ms
Structural characteristics Size     47×44×14   mm
Weight     50   g
Use environment Operating temperature   -40   80 ºC
Storage temperature   -45   85 ºC
Vibration     20~2000Hz,6.06g    
Impact     1000g,0.5ms    
Reliability MTBF     20000   h
Continuous working time     120   h
1: Calculate the zero deviation of the whole temperature change process, the temperature change rate is 1 ºC/min, and the temperature range is -40 ºC ~ + 80 ºC;
2: Vibration condition is 6.06 G, 20Hz ~ 2000Hz

Electrical interface

Three Axis Imu Accelerometer Gyro Fog Imu Inertial Measurement UnitThree Axis Imu Accelerometer Gyro Fog Imu Inertial Measurement Unit

Product Structure

Three Axis Imu Accelerometer Gyro Fog Imu Inertial Measurement Unit

Main Application Fields

Three Axis Imu Accelerometer Gyro Fog Imu Inertial Measurement Unit
Three Axis Imu Accelerometer Gyro Fog Imu Inertial Measurement Unit
Three Axis Imu Accelerometer Gyro Fog Imu Inertial Measurement Unit

Company Profile


Three Axis Imu Accelerometer Gyro Fog Imu Inertial Measurement UnitThree Axis Imu Accelerometer Gyro Fog Imu Inertial Measurement Unit



 

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Manufacturer/Factory, Trading Company
Registered Capital
1000000 RMB
Plant Area
1001~2000 square meters