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ADIS16501/PCBZ датащи(PDF) 16 Page - Analog Devices

номер детали ADIS16501/PCBZ
подробное описание детали  Precision, MEMS IMU
PDF  45 Pages
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производитель  AD [Analog Devices]
домашняя страница  http://www.analog.com
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ADIS16501/PCBZ датащи(HTML) 16 Page - Analog Devices

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Data Sheet
ADIS16501
TERMINOLOGY
analog.com
Rev. B | 16 of 45
Nonlinearity
Nonlinearity is the maximum deviation of any sensor data point
(ΩMEAS(Ωn) or ACCMEAS(gn)) from the least squares linear fit of the
sensor data at an equivalent applied angular rate or acceleration.
Nonlinearity is mathematically expressed as
Gyroscope = ΩMEAS(Ωn) – ΩCALC(Ωn)
Acceleration = ACCMEAS(gn) – ACCCALC(gn)
where:
ΩMEAS is the measured angular rate at Ωn.
ΩCALC is the linear fit calculation of the angular rate at Ωn.
ACCMEAS is the measured acceleration at gn.
ACCCALC is the linear fit calculation of acceleration at gn.
For testing across a range of ±125°/sec (gyroscope) or ±2.5 g
(accelerometer), apply the following input stimulus profile:
Ωn = −125°/sec + (n × 2.5)
where n = 0, 1, …, 100.
gn = −2.5 g + (n × 0.05)
where n = 0, 1, …, 100.
For testing across a range of ±500°/sec (gyroscope) or ±14 g
(accelerometer), apply the following input stimulus profile:
Ωn = −500°/sec + (n × 5)
where n = 0, 1, …, 200.
gn = −14 g + (n × 0.2)
where n = 0, 1, …, 100.
Figure 27. Nonlinearity Characteristic
Microlinearity
Microlinearity is the maximum deviation of the gradient between
two neighboring sensor data points as compared to the scale factor
calculated from the least squares linear fit of the sensor data.
Microlinearity is mathematically expressed as
Gyroscope= ΩMEASΩn+1−ΩMEASΩn
ΩSTEP×Sensitivity
×100%
Acceleration= ACCMEASgn+1+ACCMEASgn
gSTEP×Sensitivity
−1
×100%
where:
ΩMEAS is the measured angular rate at a defined Ωn.
ACCMEAS is the measured acceleration at a defined gn.
For testing across a range of ±125°/sec (gyroscope) or ±2.5 g
(accelerometer), apply the following input stimulus profile:
ΩSTEP = 5°/sec
gSTEP = 100 mg
Ωn = −125°/sec + (n × ΩSTEP)
where n = 0, 1, …, 50.
gn = −2.5 g + (n × gSTEP)
where n = 0, 1, …, 50.
For testing across a range of ±500°/sec (gyroscope) or ±14 g
(accelerometer), apply the following input stimulus profile:
ΩSTEP = 10°/sec
gSTEP = 250 mg
Ωn = −500°/sec + (n × ΩSTEP)
where n = 0, 1, …, 99.
gn = −14 g + (n × gSTEP)
where n = 0, 1, …, 95.



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