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ADIS16489 Datasheet(PDF) 30 Page - Analog Devices

Part # ADIS16489
Description  Seven Degrees of Freedom Inertial Sensor
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Manufacturer  AD [Analog Devices]
Direct Link  http://www.analog.com
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ADIS16489 Datasheet(HTML) 30 Page - Analog Devices

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ADIS16489
Data Sheet
Rev. B | Page 30 of 40
DECIMATION FILTER (DEC_RATE)
Table 158. DEC_RATE Register Definitions
Page
Addresses
Default
Access
Flash Backup
0x03
0x0C, 0x0D
0x0000
R/W
Yes
Table 159. DEC_RATE Bit Definitions
Bits
Description
[15:11]
Don’t care
[10:0]
Decimation rate, binary format, maximum = 2047, see
Figure 33 for the impact on sample rate
The DEC_RATE register (see Table 158 and Table 159)
provides user control for the final filter stage (see Figure 33),
which averages and decimates the accelerometers and
gyroscopes data, while also extending the time that the delta
angle and delta velocity track between each update. The output
sample rate is equal to 2460/(DEC_RATE + 1). When using the
external clock option (Bit 7 and Bits[5:4] of the FNCTIO_CTRL
register, see Figure 33), replace the 2460 number in this
relationship with the input clock frequency. For example, turn
to Page 3 (DIN = 0x8003), and set DEC_RATE = 0x18 (DIN =
0x8C18, then DIN = 0x8D00) to reduce the output sample rate to
98.4 SPS (2460 ÷ 25).
CONTINUOUS BIAS ESTIMATION (NULL_CNFG)
Table 160. NULL_CNFG Register Definitions
Page
Addresses
Default
Access
Flash Backup
0x03
0x0E, 0x0F
0x070A
R/W
Yes
Table 161. NULL_CNFG Bit Definitions
Bits
Description
[15:14]
Not used.
13
Z-axis acceleration bias correction enable (1 = enabled).
12
Y-axis acceleration bias correction enable (1 = enabled).
11
X-axis acceleration bias correction enable (1 = enabled).
10
Z-axis gyroscope bias correction enable (1 = enabled).
9
Y-axis gyroscope bias correction enable (1 = enabled).
8
X-axis gyroscope bias correction enable (1 = enabled).
[7:4]
Not used.
[3:0]
Time base control (TBC), range is 0 to 13 (default = 10),
time base (tB) = 2TBC/fS, where fS is the IMU sample rate
before decimation and is 2460 SPS if the factory default
internal clock is used. The total average time
(tA) required for autonull = 64 × tB.
The NULL_CNFG register (see Table 160 and Table 161)
provides the configuration controls for the CBE, which associates
with the bias correction update command in GLOB_CMD[0]
(see Table 151). NULL_CNFG[3:0] establish the total average
time (tA) for the bias estimates and NULL_ CNFG[13:8] provide
on/off controls for each sensor. The factory default configuration
for NULL_CNFG enables the bias null command for the
gyroscopes, disables the bias null command for the accelerometers,
and sets the average time to ~26.64 sec. This calculation assumes
that the internal sample clock (fS = 2460 SPS) is used. If the user
is supplying an external clock by setting Bit 7 of the FNCTIO_
CRTL register to 1 (see Table 152 and Table 153), fS is the IMU
sample rate before decimation.
When a sensor bit in NULL_CNFG is active (equal to 1), setting
GLOB_CMD[0] = 1 (DIN sequence: 0x8003, 0x8201, 0x8300)
causes its bias correction register to automatically update with a
value that corrects for its present bias error (from the CBE). For
example, setting NULL_CNFG[8] equal to 1 causes an update
in the XG_BIAS_LOW (see Table 109) and XG_BIAS_HIGH
(see Table 111) registers.
MEMS
SENSOR
330Hz
÷4
fs
GYROSCOPE
2-POLE: 404Hz, 757Hz
ACCELEROMETER
1-POLE: 330Hz
AVERAGE
DECIMATION
FILTER
SELECTABLE
FIR FILTER BANK
FILTR_BNK_0
FILTR_BNK_1
AVERAGE/DECIMATION FILTER
D = DEC_RATE, BITS[10:0] + 1
1
4
4
÷D
1
D
D
FIR
FILTER
BANK
fs
INTERNAL
ADC
CLOCK
9.84kHz
DIOx
OPTIONAL INPUT CLOCK
FNCTIO_CTRL, BIT 7 = 1
fs < 2400Hz
NOTES
1. WHEN FNCTIO_CTRL, BIT 7 = 1,
fs IS THE EXTERNAL INPUT CLOCK, AND EACH CLOCK PULSE ON THE DESIGNATED DIOx LINE
4× AVERAGE/DECIMATION FILTER, WHICH PRODUCES A DATA RATE THAT IS EQUAL TO THE INPUT CLOCK FREQUENCY.
2. WHEN FNCTIO_CTRL, BIT 7 = 0,
fs IS THE INTERNALLY GENERATED 2.46 kHz SAMPLE CLOCK.
(FNCTIO_CTRL, BITS[5:4]) STARTS A 4-SAMPLE BURST, AT A SAMPLE RATE OF 9.84 kHz. THESE FOUR SAMPLES FEED INTO THE
Figure 33. Sampling and Frequency Response Signal Flow


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