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Small Size Inertial Measurement Unit ADIS16488 And High Overload Resistance

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Small Size Inertial Measurement Unit ADIS16488 And High Overload Resistance

Brand Name : Firepower

Model Number : 16480G

Certification : CE ROHS

Place of Origin : CHINA

MOQ : 1

Price : negotiable

Payment Terms : T/T,L/C

Supply Ability : 500/month

Packaging Details : sponge/box

Product name : MEMS Inertial Measurement Unit

Measuring range : ±450º/s

zero bias stability : 2deg/h

Random walk : 0.1deg /√h

Zero-bias repeatability : 0.1deg/s

Bandwidth : 400Hz

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Inertial Measurement Unit ADIS16488 Small Size And High Overload Resistance IMU

 

IMU16488B is a domestic inertial measurement unit with high performance, small size and high overload resistance.

The gyro bias stability is 1.2 °/H (Allan) and the accelerometer bias stability is 50 µg (Allan). It can be used for precise

navigation, control and dynamic measurement of weapons. This series of products adopt high-precision MEMS inertial

devices, which have high reliability and high robustness, and can accurately measure the angular velocity and

acceleration information of moving carriers in harsh environments.

 

Main technical indicators

 

 

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Test conditions

Minimum value

Typical value

Maximum value
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  •  
 Measuring range  
  1.  
  1.  
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Zero bias stability Allan variance
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  1.  
  •  
 deg /h
Random walk  
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  1.  
  •  
 deg /√h
Zero-bias repeatability

 

−40°C ≤ TA ≤ +85°C

  
  1.  
  1.  
  •  
Scale factor repeatability

Full temperature range

−40°C ≤ TA ≤ +85°C

  
  1.  
  1.  
  •  
Scale factor nonlinearity FS=450 º/s  
  1.  
  1.  
  •  
  •  
      
  1.  
  •  
  •  
  •  
     ±5
  1.  
  1.  
Zero bias stability    
  1.  
  
  1.  
Random walk    
  1.  
  1.  
  •  
Zero-bias repeatability

Full temperature range

−40°C ≤ TA ≤ +85°C

  
  1.  
  1.  
  1.  
Scale factor repeatability

Full temperature range

−40°C ≤ TA ≤ +85°C

  
  1.  
  1.  
  •  
Scale factor nonlinearity    

0.1

  1.  

0.2

  1.  
  •  
  •  
      
  1.  
 Hz 3dB
  •  
 Dynamic measuring range    
  1.  

 

  
  1.  
  •  
    
  1.  
  
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Noise density    
  1.  
  
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  •  
    
  1.  
  
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  •  
 Pressure range  
  1.  
  
  1.  
  1.  
  •  
    
  1.  
  
  1.  
Absolute measurement accuracy    
  1.  
  
  1.  

Externally based

  1.  

Inertial satellite

Integrated navigation

  •  
 Heading accuracy Single GNSS, Maneuver Required, RMS  
  1.  
  
  •  
Pitch and roll accuracy GNSS Valid, RMS  
  1.  
  
  •  
GNSS invalid, unlimited time, RMS  
  1.  
  
  •  
Position accuracy GNSS Valid, Single Point L1/L2, RMS  
  1.  
  
  1.  
Speed accuracy GNSS Valid, Single Point L1/L2, RMS  
  1.  
  
  •  
Communication interface 1-way SPI Baud rate    
  1.  
  •  
1-way UART Baud rate
  1.  
  1.  
  1.  
  •  
Electrical characteristics
  •  
  
  1.  
  1.  
  1.  
  1.  
Power consumption      
  1.  
  1.  
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  •  
    
  1.  
  •  
Structural characteristics
  •  
    
  1.  
  
  1.  
  •  
        
  1.  
Use environment Operating temperature  
  1.  
  
  1.  
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Storage temperature  
  1.  
  
  1.  
  •  
  •  
    
  1. ,3g
    
  •  
    
  1. ,11ms
    
 
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 (Half-sine 0.5msec)  
  1.  
    
  •  
  1.  
    
  1.  
  
  1.  
Continuous working time    
  1.  
  
  1.  
 

IMU polarity definition

3 gyros  and 3 accelerometers  is defined as shown in the figure below, and the direction of the arrow is positive.

 


Product Tags:

Small Inertial Measurement Unit

      

ADIS16488 Inertial Measurement Unit

      

2deg/h IMU Accelerometer Gyro

      
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