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Low Drift High Performance Inertial Measurement Unit Sensor For UAVs And Intelligent Driving

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Low Drift High Performance Inertial Measurement Unit Sensor For UAVs And Intelligent Driving

Brand Name : AVIC

Model Number : GI200F-A0

Certification : CE

Place of Origin : CHINA

MOQ : 1

Price : negotiable

Payment Terms : T/T

Supply Ability : 1000/month

Delivery Time : 1 week

Packaging Details : sponge/box

Product name : IMU Accelerometer Gyro

Gryo scope : 500deg/s

Gryo allan variance : 2deg/h

Accelerometer allan variance : 0.1mg

Accelerometer scope : 16g

Communication interface : 1-channel SPI/UART

Gryo scale factor accuracy : 0.3%

Power Supply Voltage : 3.3V

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Low Drift High Performance Inertial Measurement Unit Sensor for UAVs and Intelligent Driving

Product Description

The GI200F-A0-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.

GI200F-A0-IMU has high reliability and strong environmental adaptability. By matching different software, the product can be widely used in intelligent driving, tactical and industrial UAV, intelligent ammunition, seeker, mobile communication, mapping, stable platform and other fields.

Main Application Field

  1. Intelligent driving
  2. Tactical and Industrial UAV
  3. Smart Munitions
  4. Seeker
  5. Communication in motion
  6. Mapping
  7. Stabilize the platform

Main Functions

  1. Three-axis digital gyroscope:
    1. ± 500º/s dynamic measuring range;
    2. Zero bias stability: 10 °/H (GJB, 10s), 2.0 °/H (ALLAN);
  2. Triaxial digital accelerometer:
    1. ± 16g dynamic measuring range;
    2. Zero-bias stability: 0.5mg (GJB, 10s), 0.1mg (ALLAN);
  3. High reliability: MTBF > 20000h;
  4. Guaranteed accuracy within the full temperature range (-40 ℃~ 70 ℃): built-in high-performance temperature calibration and compensation algorithm;
  5. Suitable for working under strong vibration conditions;
  6. Interface 1 channel SPI, 1 channel UART.

Performance Index

Parameter Test conditions Minimum value Typical value Maximum value Unit
Gyro Dynamic measuring range 　 500 º/s
Zero bias stability Allan variance 2 　 º/h
10 s average (-40 ℃ ~ + 70 ℃, constant temperature) 10 　 º/h
Zero bias Zero bias range ±0.5 　 º/s
Zero-bias variation over full temperature range① ±0.5 　 º/s
Scale factor Scale factor accuracy 0.3 　 %
Scale factor nonlinearity 0.02 　 %FS
Bandwidth 　 　 200 　 Hz
Accelerometer Dynamic measuring range 　 16 　 g
Zero bias stability Allan variance 0.1 　 mg
10 s average (-40 ℃ ~ + 70 ℃, constant temperature) 0.5 　 mg
Zero bias Zero bias range 2 　 mg
Zero bias change in full temperature range, peak-to-peak value① 2 　 mg
Scale factor Scale factor accuracy 0.3 　 %
Scale factor nonlinearity 0.02 　 %FS
Bandwidth 　 　 200 　 Hz
Communication interface 1-channel SPI Baud rate 15 MHz
UART Baud rate 230.4 　 Kbps
Sampling frequency SPI 1000 　 Hz
UART 　 200 1000 Hz
Electrical characteristics Voltage 　 3.3 　 V
Power consumption 　 1 W
Ripple P-P 　 　 100 mV
Structural characteristics Size 　 24×24×10 　 mm
Weight 　 　 10 　 g
Use environment Operating temperature 　 -40 70 ℃
Storage temperature 　 -45 85 ℃
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 ℃/min, and the temperature range is-40 ℃ ~ + 70 ℃;

Electrical interface

Low Drift High Performance Inertial Measurement Unit Sensor For UAVs And Intelligent Driving

Product Structure

Low Drift High Performance Inertial Measurement Unit Sensor For UAVs And Intelligent Driving

L24mm x W24mm x H10mm(L x W x H)


Product Tags:

High Performance Inertial Measurement Unit Sensor

      

Intelligent Driving Inertial Measurement Unit Sensor

      

UAVs Inertial Measurement Unit Sensor

      
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