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ADIS16501/PCBZ Datasheet(PDF) 14 Page - Analog Devices

Part # ADIS16501/PCBZ
Description  Precision, MEMS IMU
PDF  45 Pages
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Manufacturer  AD [Analog Devices]
Direct Link  http://www.analog.com
Logo AD - Analog Devices

ADIS16501/PCBZ Datasheet(HTML) 14 Page - Analog Devices

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Data Sheet
ADIS16501
TERMINOLOGY
analog.com
Rev. B | 14 of 45
Output Full-Scale Range
Output full-scale range is the guaranteed angular rate and acceler-
ation measurement range at the output of the signal chain. The
output full-scale range is specified as a minimum value and is
guaranteed across all conditions. Angular rate and acceleration
measurement are possible beyond this value. However, perform-
ance characteristics are not guaranteed.
Bias
Bias is any static (DC) error term on the output of the ADIS16501.
It is measured as the deviation from 0°/sec or 0 g without externally
applied angular rate or acceleration (including gravity). Bias is
measured after the device is soldered to the application PCB.
To reduce the influence of external physical stimuli that may exist in
the measurement system, average bias over a sufficiently long time
window. Additionally, a data rate of >1 kHz is recommended.
Gyroscope = ΩMEAS (ΩIN = 0°/sec)
To calculate accelerometer bias, take measurements at orientations
of +1 g and −1 g and calculate the average value of the two
measurements.
XL=ACCMEASgIN=+1g+ACCMEASgIN=−1g
2
Figure 21. Acceleration Sensitivity Measurement Process
Bias Error over Temperature
Bias error over temperature is the change in bias directly attrib-
uted to changes in temperature. Bias error over temperature is
measured relative to the bias at 25°C. Figure 22 shows the bias
error over temperature expected for a device with a bias at 25°C
equivalent to the initial (start of life) bias.
Bias drift over life can cause the offset measured at 25°C to
diverge from the initial (start of life) bias measured during module
manufacture. Figure 23 shows how the bias error over temperature
limits is adjusted to accommodate the divergence of the bias at
25°C and the initial bias.
Figure 22. Bias Error over Temperature, OFFINIT = OFFAT_25°C
Figure 23. Bias Error over Temperature, OFFINIT ≠ OFFAT_25°C (Change OF-
FAT_25°C to OFFAT_25°C)
Bias Repeatability
Bias repeatability describes the long-term offset behavior over a
variety of conditions. Bias repeatability represents a projection for
long-term aging, which is derived from the drift behaviors that
a sample of units exhibits throughout a 1000-hour, 110°C high
temperature operating life (HTOL) stress.
In-Run Bias Stability
In-run bias (offset) stability is a measure of how quickly gyroscope
(or accelerometer) outputs drift over time. In-run bias stability is
derived from the minimum of the Allan variance curve as follows:
Accelerometer Allan Variance(τ) =
12n−1
∑iACCMEASτi+1−ACCMEASτi2
Gyroscope Allan Variance(τ) =
12n−1
∑iΩMEASτi+1−ΩMEASτi2



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