ADIS16488A datasheet(29/35 Pages) AD

Part #	ADIS16488A

Description	Tactical Grade, Ten Degrees of Freedom Inertial Sensor

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Data Sheet

ADIS16488A

Rev. C | Page 29 of 35

Table 112. ALM_CNFG_1(Page3, Base Address = 0x22)

Bits

Description (Default = 0x0000)

15

Y-axis magnetometer alarm (1 = enabled)

14

Not used

13

Y-axis magnetometer alarm polarity (1 = greater than)

12

Y-axis magnetometer dynamic enable (1 = enabled)

11

X-axis magnetometer (1 = enabled)

10

Not used

9

X-axis magnetometer alarm polarity(1 = greater than)

8

X-axis magnetometer dynamic enable (1 = enabled)

7

Z-axis accelerometer alarm (1 = enabled)

6

Not used

5

Z-axis accelerometer alarm polarity (1 = greater than)

4

Z-axis accelerometer dynamic enable (1 = enabled)

3

Y-axis accelerometer alarm (1 = enabled)

2

Not used

1

Y-axis accelerometer alarm polarity (1 = greater than)

0

Y-axis accelerometer dynamic enable (1 = enabled)

Table 113. ALM_CNFG_2(Page3, Base Address = 0x24)

Bits

Description (Default = 0x0000)

[15:8]

Not used

7

Barometer alarm (1 = enabled)

6

Not used

5

Barometer alarm polarity (1 = greater than)

4

Barometer dynamic enable (1 = enabled)

3

Z-axis magnetometer alarm (1 = enabled)

2

Not used

1

Z-axis magnetometer alarm polarity (1 = greater than)

0

Z-axis magnetometer dynamic enable (1 = enabled)

DYNAMIC ALARM USE

The dynamicalarm settingprovidestheoptionto comparethe

change in theoutput of eachsensorover a periodof48.7 mswith

that sensor’sxx_ALM_MAGNregister.

Alarm Example

Table 114 offers an alarmconfigurationexample,which setsthe

z-axis gyroscopealarmto tripwhen Z_GYRO_OUT> 131.1°/sec

(0x199B).

Table 114. Alarm ConfigurationExample

DIN

Description

0xAC9B

Set ZG_ALM_MAGN[7:0] = 0x9B

0xAD19

Set ZG_ALM_MAGN[15:8] = 0x19

0xA000

Set ALM_CNFG_0[7:0] = 0x00

0xA103

Set ALM_CNFG_0[15:8] = 0x03

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