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6 Axis Imu Accelerometer Gyro Inertial Measure Unit High Performance Low Bias 16488 Mems Imu Accelerometer, Imu, Inertial Measurement Unit image 16 Axis Imu Accelerometer Gyro Inertial Measure Unit High Performance Low Bias 16488 Mems Imu Accelerometer, Imu, Inertial Measurement Unit image 26 Axis Imu Accelerometer Gyro Inertial Measure Unit High Performance Low Bias 16488 Mems Imu Accelerometer, Imu, Inertial Measurement Unit image 3

6 Axis Imu Accelerometer Gyro Inertial Measure Unit High Performance Low Bias 16488 Mems Imu Accelerometer, Imu, Inertial Measurement Unit

Shenzhen Avionics Technology Co., Limited

Price $2500.00 / Pieces
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Model NO.
16488H-A
Customized
Customized
Gyro Range
-450deg/S-+450deg/S
Zero Bias Stability
0.3 Deg/H
Acc Range
20g
Acc Bias Stability
2ug
Bandwidth (-3dB)
250Hz
Transport Package
Sponge and Box
Specification
47mm*44mm*15mm
HS Code
9031809090
Production Capacity
100/Month
Type:
Inertial Navigation
Output Signal Type:
Digital Output
Measuring Shaft Quantities:
9 Axis
Accuracy Grade:
0.3 Deg/H
IP Rating:
IP67
Certification:
CE
6 Axis IMU Accelerometer Gyro Inertial Measure Unit High Performance Low Bias 16488 MEMS IMU Accelerometer

This instruction manual is the main document for the operation of the 16488H inertial measurement unit. This instruction manual is mainly compiled in accordance with the Technical Specifications for Inertial Measurement Unit and Three-axis Gyroscope Unit. The 16488H 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.
 
Specifications
ParameterTest conditionsMinimum valueTypical valueMaximum valueUnit
GyroDynamic measuring range  ±450 º/s
Bias instabilityAllan variance, better than 0.3 º/h
Bias stability1s smooth, RMS, better than 10 º/h
Bias in full temperature range-40 ºC ~ 85 ºC, 10 s smoothing, RMS 0.005 º/s
Random walk1б 0.15 º/√h
Bias repeatability1б 10 º/h
Output noiseNo filtering, RMS 0.05 º/s
Scale factor repeatability1б 0.01 %
Scale factor nonlinearity1б 0.01 %
Scale factorFS=450 º/s, 32bits 2621440 LSB/°/sec
Bandwidth (-3dB)  250 Hz
Cross coupling  0.1 %
Acceleration sensitivity  1 °/h/g
Vibration rectification effect  0.5 °/h/g2
Resonant frequency  12k Hz
AccelerometerDynamic measuring range  ±20 g
Bias stabilityAllan variance 2 ug
Bias in full temperature range-40 ºC ~ 85 ºC, 10 s smoothing, RMS 1 mg
Random walk1б 0.029 m/s/√h
Bias repeatability1б 5 mg
Output noiseNo filtering, RMS 0.5 mg
Scale factor repeatability1б 0.1 %
Scale factor nonlinearityFS=20g 0.1 %FS
Scale factor±20, 32bits 65536000 g/LSB
Bandwidth (-3dB)  250 Hz
Cross coupling  0.1 %
TemperatureScale factor  0.0125 °C/LSB
Communication interface1-way SPIEnter the clock frequency 815MHz
Electrical characteristicsVoltageDirect current 3.3 ± 10% V
Power consumption  11.5W
RippleP-P 48±2100mV
Use environmentOperating temperatureScalable-40 85ºC
Storage temperature -55 85ºC
Vibration  10~2000Hz,6.06g  
Impact  1000g,0.1ms  



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6 Axis Imu Accelerometer Gyro Inertial Measure Unit High Performance Low Bias 16488 Mems Imu Accelerometer
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6 Axis Imu Accelerometer Gyro Inertial Measure Unit High Performance Low Bias 16488 Mems Imu Accelerometer6 Axis Imu Accelerometer Gyro Inertial Measure Unit High Performance Low Bias 16488 Mems Imu Accelerometer








 

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