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Small Size Inertial Measurement Unit ADIS16488 And High Overload Resistance

Categories IMU Accelerometer Gyro
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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Small Size Inertial Measurement Unit ADIS16488 And High Overload Resistance

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). 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




Test conditions

Minimum value

Typical value

Maximum value



Measuring range




Zero bias stabilityAllan variance



deg /h
Random walk



deg /√h
Zero-bias repeatability


−40°C ≤ TA ≤ +85°C





Scale factor repeatability

Full temperature range

−40°C ≤ TA ≤ +85°C





Scale factor nonlinearityFS=450 º/s













±5


Zero bias stability




Random walk




Zero-bias repeatability

Full temperature range

−40°C ≤ TA ≤ +85°C





Scale factor repeatability

Full temperature range

−40°C ≤ TA ≤ +85°C





Scale factor nonlinearity

0.1


0.2








Hz 3dB

Dynamic measuring range











Noise density











Pressure range










Absolute measurement accuracy




Externally based


Inertial satellite

Integrated navigation


Heading accuracySingle GNSS, Maneuver Required, RMS



Pitch and roll accuracyGNSS Valid, RMS



GNSS invalid, unlimited time, RMS



Position accuracyGNSS Valid, Single Point L1/L2, RMS



Speed accuracyGNSS Valid, Single Point L1/L2, RMS



Communication interface1-way SPIBaud rate



1-way UARTBaud rate




Electrical characteristics






Power consumption










Structural characteristics












Use environmentOperating temperature




Storage temperature







  1. ,3g





  1. ,11ms




(Half-sine 0.5msec)










Continuous working time





IMU polarity definition

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


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