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ADIS16501/PCBZ 데이터시트(PDF) 16 Page - Analog Devices |
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ADIS16501/PCBZ 데이터시트(HTML) 16 Page - Analog Devices |
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16 / 45 page ![]() 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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