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Adis16488 Replacement Imu Mems Sensor Optional Version Inertial Measure Unit 6 Axis Accelerometer Gyro, Imu, Inertial Measurement Unit image 1Adis16488 Replacement Imu Mems Sensor Optional Version Inertial Measure Unit 6 Axis Accelerometer Gyro, Imu, Inertial Measurement Unit image 2Adis16488 Replacement Imu Mems Sensor Optional Version Inertial Measure Unit 6 Axis Accelerometer Gyro, Imu, Inertial Measurement Unit image 3

Adis16488 Replacement Imu Mems Sensor Optional Version Inertial Measure Unit 6 Axis Accelerometer Gyro, Imu, Inertial Measurement Unit

Shenzhen Avionics Technology Co., Limited

Price $850.00 / Pieces
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-+Subtotal: $850
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Model NO.
16488C
Customized
Customized
Gyro Range
-450deg/S-+450deg/S
Zero Bias Instability
5deg/H
Gyro Zero Bias Stability
30deg/H
Acc Range
20g
Acc Zero Bias Stability
0.07mg
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:
1deg/H
IP Rating:
IP67
Certification:
CE
ADIS16488 Replacement IMU MEMS Sensor Optional Version Inertial Measure Unit 6 Axis Accelerometer Gyro

The 16488C multi-degree-of-freedom inertial measurement unit is a complete inertial system with a built-in three-axis gyroscope, a three-axis accelerometer, a three-axis magnetometer and a pressure sensor for measuring the three-axis angle of the carrier parameters such as rate, acceleration, three-axis magnetic field, air pressure, etc., output data after error compensation (including temperature compensation, installation misalignment angle compensation, nonlinear compensation, etc.) according to the communication protocol through SPI or URAT.
    parameterTest ConditionsMinimum valueTypical valueMaximumunit
GyroDynamic measuring rangeConfigurable (maximum ± 1000)±300±450±1000º/s
Zero bias instabilityAllan variance, better than 5 º/h
Zero bias stability1s smooth, rms, better than 30 º/h
Zero bias over the full temperature range-40 ºC ~ 85 ºC, 10s smooth, rms 0.03 º/s
Random walk 0.26 º/√h
Zero bias repeatability 100 º/h
Output noiseNo filtering, rms 0.135 º/s
Scale factor repeatability 0.1 %
Scale factor nonlinearityFS=450 º/s 0.01 %FS
Bandwidth (-3dB)  330 Hz
Cross coupling  0.1 %
AccelerometerDynamic measuring rangeConfigurable (maximum ± 40)±18±20±40g
Zero bias stabilityAllan variance 0.07 mg
Zero bias over the full temperature range-40 ºC ~ 85 ºC, 10s smooth, rms 5 mg
Random walk 0.029 m/s/√h
Zero bias repeatability 16 mg
Output noiseNo filtering, rms 1 mg
Scale factor repeatability 0.1 %
Scale factor nonlinearityFS=10g 0.1 %FS
Bandwidth (-3dB)  330 Hz
Cross coupling  0.1 %
MagnetometerDynamic measuring range  ±2.5 gauss
Sensitivity  0.1 mgauss/LSB
Nonlinearity  0.5 %FS
BarometerPressure range 300 1100mbar
Sensitivity  6.1 × 10-7 mbar/LSB
Total error  4.5 mbar
Relative error  2.5 mbar
Nonlinearity  0.1 %FS
Communication Interface1 way spiInput clock frequency  15MHz
1 way uartBaud rate9.6614.4921.6kbps
Electrical characteristicsVoltageDC 3.3 (or 5) ± 10% V
Power consumption  0.61W
RippleP-P  100mV
weight  48±2 g
Use environmentOperating temperatureScalable-40 85ºC
storage temperature -55 85ºC
vibration  10~2000Hz,6.06g  
Shock  5000g,0.1ms  

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Adis16488 Replacement Imu Mems Sensor Optional Version Inertial Measure Unit 6 Axis Accelerometer Gyro
Company and production line
Adis16488 Replacement Imu Mems Sensor Optional Version Inertial Measure Unit 6 Axis Accelerometer Gyro
Adis16488 Replacement Imu Mems Sensor Optional Version Inertial Measure Unit 6 Axis Accelerometer Gyro

 

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