LSM9DS1 Datasheet, PDF (50/72 Pages) –

Accelerometer and gyroscope register description
LSM9DS1
IG_XL
IG_G
INACT
BOOT_
STATUS
TDA
GDA
XLDA
Table 61. STATUS_REG register description
Accelerometer interrupt output signal. Default value: 0
(0: no interrupt has been generated; 1: one or more interrupt events have been gener-
ated)
Gyroscope interrupt output signal. Default value: 0
(0: no interrupt has been generated; 1: one or more interrupt events have been gener-
ated)
Inactivity interrupt output signal. Default value: 0
(0: no interrupt has been generated; 1: one or more interrupt events have been gener-
ated)
Boot running flag signal. Default value: 0
(0: no boot running; 1: boot running)
Temperature sensor new data available. Default value: 0
(0: new data is not yet available; 1: new data is available)
Gyroscope new data available. Default value: 0
(0: a new set of data is not yet available; 1: a new set of data is available)
Accelerometer new data available. Default value: 0
(0: a new set of data is not yet available; 1: a new set of data is available)
7.19
7.20
7.21
7.22
OUT_X_G (18h - 19h)
Angular rate sensor pitch axis (X) angular rate output register. The value is expressed as a
16-bit word in two’s complement.
OUT_Y_G (1Ah - 1Bh)
Angular rate sensor roll axis (Y) angular rate output register. The value is expressed as a
16-bit word in two’s complement.
OUT_Z_G (1Ch - 1Dh)
Angular rate sensor Yaw axis (Z) angular rate output register. The value is expressed as a
16-bit word in two’s complement.
CTRL_REG4 (1Eh)
Control register 4.
Table 62. CTRL_REG4 register
0⁽¹⁾
0⁽¹⁾
Zen_G Yen_G Xen_G
0⁽¹⁾
1. These bits must be set to ‘0’ for the correct operation of the device.
LIR_XL1 4D_XL1
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