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ADIS16489 Datasheet(PDF) 32 Page - Analog Devices

Part No. ADIS16489
Description  Seven Degrees of Freedom Inertial Sensor
Download  40 Pages
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Manufacturer  AD [Analog Devices]
Direct Link  http://www.analog.com
Logo AD - Analog Devices

ADIS16489 Datasheet(HTML) 32 Page - Analog Devices

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ADIS16489
Data Sheet
Rev. B | Page 32 of 40
Solving for ΔX_ACCL_OUT, ΔZ_GYRO_OUT,
ΔY_GYRO_OUT, and ΔX_GYRO_OUT
Use Equation 1 to Equation 4 to solve for ΔX_ACCL_OUT,
ΔZ_GYRO_OUT, ΔY_GYRO_OUT, and ΔX_GYRO_OUT,
which the following bits provide user control for in the
ALM_CFG_0 register (see Table 170) in Bits[13:12], Bits[9:8],
Bits[5:4], and Bits[1:0].
( )
(
)
−
−
=
∑
∑
=
=
7
0
7
0
112
8
1
n
A
n
A
n
X
n
X
T
ΔX_ACCL_OU
(1)
where XA = X_ACCL_OUT.
( )
(
)
−
−
=
∑
∑
=
=
7
0
7
0
112
8
1
n
G
n
G
n
Z
n
Z
T
ΔZ_GYRO_OU
(2)
where ZG = Z_GYRO_OUT.
( )
(
)
−
−
=
∑
∑
=
=
7
0
7
0
112
8
1
n
G
n
G
n
Y
n
Y
T
ΔY_GYRO_OU
(3)
where YG = Y_GYRO_OUT.
( )
(
)
−
−
=
∑
∑
=
=
7
0
7
0
112
8
1
n
G
n
G
n
X
n
X
T
ΔX_GYRO_OU
(4)
where XG = X_GYRO_OUT.
Table 170. ALM_CNFG_0 Bit Definitions
Bits
Description
15
X-axis accelerometer; 0: alarm is off, 1: alarm is on
14
Not used
[13:12]
X-axis accelerometer polarity and mode settings; select
one of the four options for the condition that triggers
the alarm (ALM_STS[3] = 1, see Table 20)
00: X_ACCL_OUT < XA_ALM_MAGN
01: ΔX_ACCL_OUT < XA_ALM_MAGN (see Equation 1)
10: X_ACCL_OUT > XA_ALM_MAGN
11: ΔX_ACCL_OUT > XA_ALM_MAGN (see Equation 1)
11
Z-axis gyroscope; 0: alarm is off, 1: alarm is on
10
Not used
[9:8]
Z-axis gyroscope polarity and mode settings; select
one of the four options for the condition that triggers
the alarm (ALM_STS[2] = 1, see Table 20)
00: Z_GYRO_OUT < ZG_ALM_MAGN
01: ΔZ_GYRO_OUT < ZG_ALM_MAGN (see Equation 2)
10: Z_GYRO_OUT > ZG_ALM_MAGN
11: ΔZ_GYRO_OUT > ZG_ALM_MAGN (see Equation 2)
7
Y-axis gyroscope; 0: alarm is off, 1: alarm is on
6
Not used
[5:4]
Y-axis gyroscope polarity and mode settings. Select
one of the four options for the condition that triggers
the alarm (ALM_STS[1] = 1, see Table 20)
00: Y_GYRO_OUT < YG_ALM_MAGN
01: ΔY_GYRO_OUT < YG_ALM_MAGN (see Equation 3)
10: Y_GYRO_OUT > YG_ALM_MAGN
11: ΔY_GYRO_OUT > YG_ALM_MAGN (see Equation 3)
3
X-axis gyroscope; 0: alarm is off, 1: alarm is on
Bits
Description
2
Not used
1:0
X-axis gyroscope polarity and mode settings; select
one of the four options for the condition that triggers
the alarm flag (ALM_STS[0] = 1, see Table 20)
00: X_GYRO_OUT < XG_ALM_MAGN
01: ΔX_GYRO_OUT < XG_ALM_MAGN (see Equation 4)
10: X_GYRO_OUT > XG_ALM_MAGN
11: ΔX_GYRO_OUT > XG_ALM_MAGN (see Equation 4)
Table 171. ALM_CNFG_1 Register Definitions
Page
Addresses
Default
Access
Flash Backup
0x03
0x22, 0x23
0x0000
R/W
Yes
Solving for ΔZ_ACCL_OUT and ΔY_ACCL_OUT
Use Equation 5 and Equation 6 to solve for ΔZ_ACCL_OUT
and ΔY_ACCL_OUT in Bits[5:4] and Bits[1:0] in Table 172.
( )
(
)
−
−
=
∑
∑
=
=
7
0
7
0
112
8
1
n
A
n
A
n
Z
n
Z
T
ΔZ_ACCL_OU
(5)
where ZA = Z_ACCL_OUT.
( )
(
)
−
−
=
∑
∑
=
=
7
0
7
0
112
8
1
n
A
n
A
n
Y
n
Y
T
ΔY_ACCL_OU
(6)
where YA = Y_ACCL_OUT.
Table 172. ALM_CNFG_1 Bit Definitions
Bits
Description
[15:8]
Not used
7
Z-axis accelerometer; 0: alarm is off, 1: alarm is on
6
Not used
[5:4]
Z-axis accelerometer polarity and mode settings; select
one of the four options for the condition that triggers
the alarm (ALM_STS[5] = 1, see Table 20)
00: Z_ACCL_OUT < ZA_ALM_MAGN
01: ΔZ_ACCL_OUT < ZA_ALM_MAGN (see Equation 5)
10: Z_ACCL_OUT > ZA_ALM_MAGN
11: ΔZ_ACCL_OUT > ZA_ALM_MAGN (see Equation 5)
4
Z-axis accelerometer mode, 0: static, 1: dynamic
3
Y-axis accelerometer; 0: alarm is off, 1: alarm is on
2
Not used
[1:0]
Y-axis accelerometer polarity and mode settings; select
one of the four options for the condition that triggers
the alarm (ALM_STS[4] = 1, see Table 20)
00: Y_ACCL_OUT < YA_ALM_MAGN
01: ΔY_ACCL_OUT < YA_ALM_MAGN (see Equation 6)
10: Y_ACCL_OUT > YA_ALM_MAGN
11: ΔY_ACCL_OUT > YA_ALM_MAGN (see Equation 6)
Table 173. ALM_CNFG_2 Register Definitions
Page
Addresses
Default
Access
Flash Backup
0x03
0x24, 0x25
0x0000
R/W
Yes


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