LSM6DS3US Datasheet, PDF (22/104 Pages) STMicroelectronics – iNEMO inertial module: always-on 3D accelerometer and 3D gyroscope

Module specifications
LSM6DS3US
6. Gyro noise RMS is independent of the ODR and FS setting.
7. Noise density in HP mode is the same for all ODRs.
8. Noise RMS in Normal/LP mode is the same for all the ODR RMS related to BW = ODR /2 (for ODR /9, typ value can be
calculated by Typ *0.6)
9. To enable this ODR, refer to CTRL4_C (13h).
10. The sign of the linear acceleration self-test output change is defined by the STx_XL bits in CTRL5_C (14h), Table 60 for all
the axes.
11. The linear acceleration self-test output change is defined with the device in stationary condition as the absolute value of:
OUTPUT[LSb] (self-test enabled) - OUTPUT[LSb] (self-test disabled). 1LSb = 0.061 mg at ±2 g full scale.
12. The sign of the angular rate self-test output change is defined by the STx_G bits in CTRL5_C (14h), Table 59 for all the
axes.
13. The angular rate self-test output change is defined with the device in stationary condition as the absolute value of:
OUTPUT[LSb] (self-test enabled) - OUTPUT[LSb] (self-test disabled). 1LSb = 70 mdps at ±2000 dps full scale.
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