Flight Control Imu Sensor Low Drfit Inertial Sensor Replace 16497

Product Details
Customization: Available
After-sales Service: 1 Year
Warranty: 1 Year
Diamond Member Since 2025

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  • Flight Control Imu Sensor Low Drfit Inertial Sensor Replace 16497
  • Flight Control Imu Sensor Low Drfit Inertial Sensor Replace 16497
  • Flight Control Imu Sensor Low Drfit Inertial Sensor Replace 16497
  • Flight Control Imu Sensor Low Drfit Inertial Sensor Replace 16497
  • Flight Control Imu Sensor Low Drfit Inertial Sensor Replace 16497
  • Flight Control Imu Sensor Low Drfit Inertial Sensor Replace 16497
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  • Overview
  • Product Description
  • Technical Parameter
  • Details Images
  • Outline Drawing
  • Factory Photos
  • Company Profile
Overview

Basic Info.

Model NO.
16488HA
Gyro Scale Factor Repeatability
0.01%
Accelerometer Bias Repeatability
5mg
Customized Support
OEM,ODM
Zero Bias Stability
0.3 Deg/H
Gyro Range
500deg/S
Output Noise
0.05deg/S
Brand Name
Firepower
Acc Range
20g
Bandwidth
250Hz
Power
3.3 10V
Communication Interface
1-Channel Spi
Transport Package
Sponge and Carton
Specification
47mm*44mm*15mm
Trademark
Firepower
Origin
Shenzhen

Product Description

Product Description
The 16488HA inertial measurement unit is a complete inertial system with a built-in three-axis gyroscope and a three-axis
accelerometer, which is used to measure the three-axis angular rate, acceleration and other parameters of the carrier, and output the data after error compensation including temperature compensation, installation misalignment angle compensation, nonlinear compensation, etc.) through SPI according to the communication protocol
Technical Parameter
 
Parameter Test conditions Minimum value Typical value Maximum value Unit
Gyroscope Dynamic measuring range     ±450   º/s
Zero-bias instability Allan variance, better than   0.3   º/h
Zero bias stability 10s smooth, RMS, better than   3   º/h
Zero bias in full temperature range -40 ºC ~ 85 ºC, 10 s smooth,
rms
  20   º/h
Random walk 1σ   0.15   º/√h
Zero-bias repeatability 1σ   5   º/h
Scale factor repeatability 1σ   100   ppm
Scale factor nonlinearity 1σ   100   ppm
Bandwidth (-3dB)     250   Hz
Cross coupling     0.1   %
Resolution     2   º/h
Acceleration sensitivity     2   °/h/g
Accelerometer Dynamic measuring range     ±20   g
Zero bias stability Allan variance   0.07   mg
           
Zero bias in full temperature range -40 ºC ~ 85 ºC, 10 s smooth,
rms
  3   mg
Zero bias stability 10s smooth, RMS, better than   0.25   mg
Random walk 1σ   0.029   m/s/√h
Zero-bias repeatability 1σ   0.5   mg
Scale factor repeatability 1σ   500   ppm
Scale factor nonlinearity FS=20g   500   ppm
Bandwidth (-3dB)     250   Hz
Cross coupling     0.1   %

Communication
Interface

1-way SPI

Enter the clock frequency
 
8

15

MHz
Electrical characteristics Voltage Direct current   3.3   V
Power consumption     1.5 1.5 W
Ripple P-P   48±2 100 mV
Use environment Operating temperature   -45   85 ºC
Storage temperature   -55   85 ºC
Details Images
Flight Control Imu Sensor Low Drfit Inertial Sensor Replace 16497
Flight Control Imu Sensor Low Drfit Inertial Sensor Replace 16497
Outline Drawing
Flight Control Imu Sensor Low Drfit Inertial Sensor Replace 16497
 
Factory Photos
Flight Control Imu Sensor Low Drfit Inertial Sensor Replace 16497
Company Profile
Flight Control Imu Sensor Low Drfit Inertial Sensor Replace 16497
Flight Control Imu Sensor Low Drfit Inertial Sensor Replace 16497
Flight Control Imu Sensor Low Drfit Inertial Sensor Replace 16497
Flight Control Imu Sensor Low Drfit Inertial Sensor Replace 16497
Flight Control Imu Sensor Low Drfit Inertial Sensor Replace 16497
 

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