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LSM6DS3H Datasheet, PDF (67/104 Pages) STMicroelectronics – always-on 3D accelerometer and 3D gyroscope
LSM6DS3H
Register description
9.28
OUTX_L_G (22h)
Angular rate sensor pitch axis (X) angular rate output register (r). The value is expressed as
a 16-bit word in two’s complement.
If this register is read by the primary interface, data are according to the full scale and ODR
settings (CTRL2_G (11h)) of gyro user interface.
If this register is read by the auxiliary interface, data are according to the full scale (250 dps)
and ODR (3.33 kHz) settings of the OIS gyro.
D7
D[7:0]
Table 89. OUTX_L_G register
D6
D5
D4
D3
D2
D1
D0
Table 90. OUTX_L_G register description
Pitch axis (X) angular rate value (LSbyte)
D[15:0] expressed in two’s complement and its value depends on the interface used:
SPI1/I2C: Gyro UI chain pitch axis output
SPI2: Gyro OIS chain pitch axis output
9.29
OUTX_H_G (23h)
Angular rate sensor pitch axis (X) angular rate output register (r). The value is expressed as
a 16-bit word in two’s complement.
If this register is read by the primary interface, data are according to the full scale and ODR
settings (CTRL2_G (11h)) of gyro user interface.
If this register is read by the auxiliary interface, data are according to the full scale (250 dps)
and ODR (3.33 kHz) settings of the OIS gyro.
D15
D[15:8]
Table 91. OUTX_H_G register
D14
D13
D12
D11
D10
D9
D8
Table 92. OUTX_H_G register description
Pitch axis (X) angular rate value (MSbyte)
D[15:0] expressed in two’s complement and its value depends on the interface used:
SPI1/I2C: Gyro UI chain pitch axis output
SPI2: Gyro OIS chain pitch axis output
9.30
OUTY_L_G (24h)
Angular rate sensor roll axis (Y) angular rate output register (r). The value is expressed as a
16-bit word in two’s complement.
If this register is read by the primary interface, data are according to the full scale and ODR
settings (CTRL2_G (11h)) of gyro user interface.
If this register is read by the auxiliary interface, data are according to the full scale (250 dps)
and ODR (3.33 kHz) settings of the OIS gyro.
DocID028370 Rev 4
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