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ADIS16IMU1/PCBZ Datasheet(PDF) 26 Page - Analog Devices

Part # ADIS16IMU1/PCBZ
Description  Six Degrees of Freedom Inertial Sensor
PDF  38 Pages
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Manufacturer  AD [Analog Devices]
Direct Link  http://www.analog.com
Logo AD - Analog Devices

ADIS16IMU1/PCBZ Datasheet(HTML) 26 Page - Analog Devices

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ADIS16486
Data Sheet
Rev. 0 | Page 26 of 38
Flash Memory Endurance Counter, FLSHCNT_LOW,
FLSHCNT_HIGH
The FLSHCNT_LOW (see Table 136 and Table 137) and
FLSHCNT_HIGH (see Table 138 and Table 139) registers
combine to create a 32-bit binary counter that tracks the number
of flash memory write cycles. In addition to the number of
write cycles, the flash memory has a finite service lifetime,
which depends on the junction temperature. Figure 27 provides
guidance for estimating the retention life for the flash memory
at specific junction temperatures. The junction temperature is
approximately 7°C above the case temperature.
Table 136. FLSHCNT_LOW Register Definition
Page ID
Addresses
Default
Access
Flash Backup
0x02
0x7C, 0x7D
Not applicable
R/W
Yes
Table 137. FLSHCNT_LOW Bit Definition
Bits
Description (No Default)
[15:0]
Flash memory write counter, low word
Table 138. FLSHCNT_HIGH Register Definition
Page ID
Addresses
Default
Access
Flash Backup
0x02
0x7E, 0x7F
Not applicable
R/W
Yes
Table 139. FLSHCNT_HIGH Bit Definition
Bits
Description (No Default)
[15:0]
Flash memory write counter, high word
600
450
300
150
0
30
40
JUNCTION TEMPERATURE (°C)
55
70
85
100
125
135
150
Figure 27. Flash Memory Retention
Global Commands, GLOB_CMD
The GLOB_CMD register (see Table 140 and Table 141) provides
trigger bits for several operations. Write a 1 to the appropriate
bit in the GLOB_CMD register to start a desired function.
Table 140. GLOB_CMD Register Definition
Page ID
Addresses
Default
Access
Flash Backup
0x03
0x02, 0x03
0x0000
W
No
Table 141. GLOB_CMD Bit Definitions
Bits
Description (Default = 0x0000)
[15:8]
Not used
7
Software reset
6
Factory calibration restore
[5:4]
Not used
3
Flash memory update
2
Not used
1
Self test
0
Bias correction update
Software Reset
Select Page 3 (DIN = 0x8003) and set GLOB_CMD, Bit 7 = 1
(DIN = 0x8280, then DIN = 0x8300) to initiate a reset of the
ADIS16486. This reset removes all data, initializes all of the
registers from their flash settings, and restarts data sampling
and processing. This function provides a firmware alternative
to providing a low pulse on the RST pin (see Table 6).
Factory Calibration Restore
Select Page 3 (DIN = 0x8003) and set GLOB_CMD, Bit 6 = 1
(DIN = 0x8240, then DIN = 0x8300) to restore the factory
calibration. This restoration writes 0x0000 to the following
registers: X_GYRO_SCALE, Y_GYRO_SCALE,
Z_GYRO_SCALE, X_ACCL_SCALE, Y_ACCL_SCALE,
Z_ACCL_SCALE, XG_BIAS_LOW, XG_BIAS_HIGH,
YG_BIAS_LOW, YG_BIAS_HIGH, ZG_BIAS_LOW,
ZG_BIAS_HIGH, XA_BIAS_LOW, XA_BIAS_HIGH,
YA_BIAS_LOW, YA_BIAS_HIGH, ZA_BIAS_LOW, and
ZA_BIAS_HIGH.
Flash Memory Update
Select Page 3 (DIN = 0x8003) and set GLOB_CMD, Bit 3 = 1
(DIN = 0x8208, then DIN = 0x8300) to initiate a manual flash
update. SYS_E_FLAG, Bit 6 (see Table 20) identifies success (0)
or failure (1) in completing this process.
ODST
Select Page 3 (DIN = 0x8003) and set GLOB_CMD, Bit 1 = 1
(DIN = 0x8202, then DIN = 0x8300) to run the ODST routine,
which executes the following steps:
1. Measure the output on each sensor.
2. Activate an internal force on the mechanical elements of
each sensor, which simulates the force associated with
actual inertial motion.
3. Measure the output response on each sensor.
4. Deactivate the internal force on each sensor.
5. Calculate the difference between the force on and normal
operating conditions (force off).
6. Compare the difference with internal pass and fail criteria.
7. Report the pass and fail results for each sensor in DIAG_
STS (see Table 22) and the overall pass and fail flag in SYS_
E_FLAG, Bit 5 (see Table 20).



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