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

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

Brand Name: Firepower
Model Number: GI200F-A0
MOQ: 1
Price: negotiable
Payment Terms: T/T
Supply Ability: 1000/month
Detail Information
Place of Origin:
CHINA
Certification:
CE
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
Packaging Details:
sponge/box
Supply Ability:
1000/month
Highlight:

High Performance Inertial Measurement Unit Sensor

,

Intelligent Driving Inertial Measurement Unit Sensor

,

UAVs Inertial Measurement Unit Sensor

Product Description

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 0

 

 

Product Structure

 

Low Drift High Performance Inertial Measurement Unit  Sensor For UAVs And Intelligent Driving 1

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