Six Degrees of Freedom Inertial Sensor
Data Sheet
ADIS16360/ADIS16365
Rev. E
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FEATURES
Triaxis digital gyroscope with digital range scaling
±75°/sec, ±150°/sec, ±300°/sec settings
Tight orthogonal alignment: <0.05°
Triaxis digital accelerometer: ±18 g
Autonomous operation and data collection
No external configuration commands required
Start-up time: 180 ms
Sleep mode recovery time: 4 ms
Factory-calibrated sensitivity, bias, and axial alignment
Calibration temperature range
ADIS16360: +25°C
ADIS16365: −40°C to +85°C
SPI-compatible serial interface
Wide bandwidth: 330 Hz
Embedded temperature sensor
Programmable operation and control
Automatic and manual bias correction controls
Bartlett window, FIR filter length, number of taps
Digital I/O: data ready, alarm indicator, general-purpose
Alarms for condition monitoring
Sleep mode for power management
DAC output voltage
Enable external sample clock input: up to 1.2 kHz
Single-command self-test
Single-supply operation: 4.75 V to 5.25 V
2000 g shock survivability
Operating temperature range: −40°C to +105°C
APPLICATIONS
Medical instrumentation
Robotics
Platform controls
Navigation
GENERAL DESCRIPTION
The ADIS16360/ADIS16365 iSensor® devices are complete inertial
systems that include a triaxis gyroscope and triaxis accelerometer.
Each sensor in the ADIS16360/ADIS16365 combines industry-
leading iMEMS® technology with signal conditioning that optimizes
dynamic performance. The factory calibration characterizes each
sensor for sensitivity, bias, alignment, and linear acceleration (gyro
bias). As a result, each sensor has its own dynamic compensation
formulas that provide accurate sensor measurements.
The ADIS16360/ADIS16365 provide a simple, cost-effective
method for integrating accurate, multiaxis inertial sensing into
industrial systems, especially when compared with the complexity
and investment associated with discrete designs. All necessary
motion testing and calibration are part of the production process
at the factory, greatly reducing system integration time. Tight
orthogonal alignment simplifies inertial frame alignment in naviga-
tion systems. An improved SPI interface and register structure
provide faster data collection and configuration control.
The ADIS16360/ADIS16365 use a compatible pinout and the same
package as the ADIS1635x family. Therefore, systems that currently
use the ADIS1635x family can upgrade their performance with
minor firmware adjustments in their processor designs. These
compact modules are approximately 23 mm × 23 mm × 23 mm
and provide a flexible connector interface that enables multiple
mounting orientation options.
FUNCTIONAL BLOCK DIAGRAM
TRI-AXIS MEMS
ANGUL AR RATE
SENSOR SIGNAL
CONDITIONING
AND
CONVERSION
CALIBRATION
AND
DIGITAL
PROCESSING
DIGITAL
CONTROL
POWER
MANAGEMENT
OUTPUT
REGISTERS
AND SPI
INTERFACE
AUX_ADC AUX_DAC
RST
CS
SCLK
DIN
DOUT
TRI-AXIS MEMS
ACCELERATION
SENSOR
VCC
GND
DIO4/CLKIN
SELF-TEST
ADIS16360/
ADIS16365
TEMPERATURE
SENSOR
ALARMS
DIO3
DIO2DIO1
07570-001
Figure 1.
ADIS16360/ADIS16365 Data Sheet
Rev. E | Page 2 of 20
TABLE OF CONTENTS
Features .............................................................................................. 1
Applications ....................................................................................... 1
General Description ......................................................................... 1
Functional Block Diagram .............................................................. 1
Revision History ............................................................................... 2
Specifications ..................................................................................... 3
Timing Specifications .................................................................. 5
Timing Diagrams .......................................................................... 5
Absolute Maximum Ratings ............................................................ 6
ESD Caution .................................................................................. 6
Pin Configuration and Function Descriptions ............................. 7
Typical Performance Characteristics ............................................. 8
Theory of Operation ........................................................................ 9
Basic Operation ............................................................................ 9
Reading Sensor Data .................................................................... 9
Device Configuration .................................................................. 9
Memory Map .............................................................................. 10
Burst Read Data Collection ...................................................... 11
Output Data Registers................................................................ 11
Calibration................................................................................... 12
Operational Control ................................................................... 12
Input/Output Functions ............................................................ 14
Diagnostics .................................................................................. 15
Product Identification ................................................................ 16
Applications Information .............................................................. 17
Installation/Handling................................................................. 17
Gyroscope Bias Optimization ................................................... 17
Input ADC Channel ................................................................... 17
Interface Printed Circuit Board (PCB) .................................... 17
Outline Dimensions ....................................................................... 18
Ordering Guide .......................................................................... 18
REVISION HISTORY
9/12—Rev. D to Rev. E
Change to Device Configuration Section ...................................... 9
2/11—Rev. C to Rev. D
Changes to Gyroscopes Misalignment and Accelerometers
Misalignment Test Conditions/Comments, Table 1 .................... 3
Changes to Table 30 and Table 31 ................................................ 16
8/10—Rev. B to Rev. C
Changes to Figure 11 ........................................................................ 9
Changes to Table 8 .......................................................................... 10
Changes to Burst Read Data Collection Section ........................ 11
Changes to Internal Sample Rate Section.................................... 12
Changes to Product Identification Section and Table 32 .......... 16
12/09—Rev. A to Rev. B
Reorganized Layout ............................................................ Universal
Changes to Features Section............................................................ 1
Changes to Table 1 ............................................................................ 3
Changes to Table 2 ............................................................................ 5
Changes to Table 5 ............................................................................ 7
Changes to Table 7 and Device Configuration Section ............... 9
Changes to Table 8 .......................................................................... 10
Changes to Burst Read Data Collection Section, Output
Data Registers Section, and Table 9 ............................................. 11
Added Table 10, Table 11, Table 12, Table 13, and Table 14;
Renumbered Tables Sequentially ................................................. 11
Added Sensor Bandwidth Section and Figure 14;
Renumbered Figures Sequentially ................................................ 13
Changes to Digital Filtering Section ............................................ 13
Changes to General-Purpose I/O Section ................................... 14
Changes to Table 26 ....................................................................... 15
Changes to Table 29 and Table 31 ................................................ 16
Added Product Identification Section ......................................... 16
Added Applications Information Section, Figure 16, Figure 17,
and Figure 18; Renumbered Figures Sequentially ..................... 17
4/09—Rev. 0 to Rev. A
Changes to Features Section ............................................................ 1
Changes to Scale Factor, Table 1 ...................................................... 3
Changes to Figure 5 and Figure 6 .................................................... 7
Changes to Figure 7 and Figure 8 .................................................... 8
Changes to Device Configuration Section ..................................... 9
Changes to Figure 12 ...................................................................... 10
Changes to Operational Control Section .................................... 12
1/09—Revision 0: Initial Version
Data Sheet ADIS16360/ADIS16365
Rev. E | Page 3 of 20
SPECIFICATIONS
TA = 25°C, VCC = 5.0 V, angular rate = 0°/sec, dynamic range = ±300°/sec ± 1 g, unless otherwise noted.
Table 1.
Parameter Test Conditions/Comments Min Typ Max Unit
GYROSCOPES
Dynamic Range ±300 ±350 °/sec
Initial Sensitivity Dynamic range = ±300°/sec 0.0495 0.05 0.0505 °/sec/LSB
Dynamic range = ±150°/sec 0.025 °/sec/LSB
Dynamic range = ±75°/sec 0.0125 °/sec/LSB
Sensitivity Temperature Coefficient ADIS16360, −40°C ≤ T
A
≤ +85°C ±350 ppm/°C
ADIS16365, −40°C ≤ TA ≤ +85°C
±40
ppm/°C
Misalignment Axis-to-axis ±0.05 Degrees
Axis-to-frame (package) ±0.5 Degrees
Nonlinearity Best fit straight line ±0.1 % of FS
Initial Bias Error ±1 σ ±3 °/sec
In-Run Bias Stability 1 σ, SMPL_PRD = 0x0001 0.007 °/sec
Angular Random Walk 1 σ, SMPL_PRD = 0x0001 2.0 °/√hr
Bias Temperature Coefficient ADIS16360, −40°C ≤ T
A
≤ +85°C ±0.025 °/sec/°C
ADIS16365, −40°C ≤ T
A
≤ +85°C ±0.01 °/sec/°C
Linear Acceleration Effect on Bias Any axis, 1 σ (MSC_CTRL[7] = 1) 0.05 °/sec/g
Bias Voltage Sensitivity VCC = 4.75 V to 5.25 V ±0.3 °/sec/V
Output Noise ±300°/sec range, no filtering 0.8 °/sec rms
Rate Noise Density f = 25 Hz, ±300°/sec range, no filtering 0.044 °/sec/√Hz rms
3 dB Bandwidth 330 Hz
Sensor Resonant Frequency 14.5 kHz
Self-Test Change in Output Response ±300°/sec range setting ±696 ±1400 ±2449 LSB
ACCELEROMETERS Each axis
Dynamic Range ±18 g
Initial Sensitivity 3.285 3.33 3.38 mg/LSB
Sensitivity Temperature Coefficient ADIS16360, −40°C ≤ T
A
≤ +85°C ±120 ppm/°C
ADIS16365, −40°C ≤ T
A
≤ +85°C ±50 ppm/°C
Misalignment Axis-to-axis 0.2 Degrees
Axis-to-frame (package) ±0.5 Degrees
Nonlinearity Best fit straight line 0.1 % of FS
Initial Bias Error ±1 σ ±50 mg
In-Run Bias Stability 1 σ 0.2 mg
Velocity Random Walk 1 σ 0.2 m/sec/√hr
Bias Temperature Coefficient ADIS16360, −40°C ≤ T
A
≤ +85°C
±4 mg/°C
ADIS16365, −40°C ≤ T
A
≤ +85°C
±0.3 mg/°C
Bias Voltage Sensitivity VCC = 4.75 V to 5.25 V 2.5 mg/V
Output Noise No filtering 9 mg rms
Noise Density
No filtering
0.5
m
g
/√Hz rms
3 dB Bandwidth 330 Hz
Sensor Resonant Frequency 5.5 kHz
Self-Test Change in Output Response X-axis and y-axis 59 151 LSB
TEMPERATURE SENSOR
Scale Factor Output = 0x0000 at 25°C (±5°C) 0.136 °C/LSB
ADC INPUT
Resolution 12 Bits
Integral Nonlinearity ±2 LSB
Differential Nonlinearity ±1 LSB
Offset Error ±4 LSB
ADIS16360/ADIS16365 Data Sheet
Rev. E | Page 4 of 20
Parameter Test Conditions/Comments Min Typ Max Unit
Gain Error ±2 LSB
Input Range 0 3.3 V
Input Capacitance During acquisition 20 pF
DAC OUTPUT 5 kΩ/100 pF to GND
Resolution 12 Bits
Relative Accuracy 101 LSB ≤ input code ≤ 4095 LSB ±4 LSB
Differential Nonlinearity ±1 LSB
Offset Error ±5 mV
Gain Error ±0.5 %
Output Range 0 3.3 V
Output Impedance 2 Ω
Output Settling Time 10 µs
LOGIC INPUTS
1
Input High Voltage, V
IH
2.0 V
Input Low Voltage, V
IL
0.8 V
CS
signal to wake up from sleep mode
0.55
V
CS Wake-Up Pulse Width 20 µs
Logic 1 Input Current, I
IH
V
IH
= 3.3 V ±0.2 ±10 µA
Logic 0 Input Current, I
IL
V
IL
= 0 V
All Pins Except RST 40 60 μA
RST Pin 1 mA
Input Capacitance, CIN
10
pF
DIGITAL OUTPUTS1
Output High Voltage, V
OH
I
SOURCE
= 1.6 mA 2.4 V
Output Low Voltage, V
OL
I
SINK
= 1.6 mA 0.4 V
FLASH MEMORY Endurance2 10,000 Cycles
Data Retention3 T
J
= 85°C 20 Years
FUNCTIONAL TIMES4 Time until data is available
Power-On Start-Up Time Normal mode, SMPL_PRD ≤ 0x09 180 ms
Low power mode, SMPL_PRD ≥ 0x0A 250 ms
Reset Recovery Time Normal mode, SMPL_PRD ≤ 0x09 60 ms
Low power mode, SMPL_PRD ≥ 0x0A 130 ms
Sleep Mode Recovery Time Normal mode, SMPL_PRD ≤ 0x09 4 ms
Low power mode, SMPL_PRD ≥ 0x0A 9 ms
Flash Memory Test Time
Normal mode, SMPL_PRD ≤ 0x09
17
ms
Low power mode, SMPL_PRD ≥ 0x0A 90 ms
Automatic Self-Test Time SMPL_PRD = 0x0001 12 ms
CONVERSION RATE SMPL_PRD = 0x0001 to 0x00FF 0.413 819.2 SPS
Clock Accuracy ±3 %
Sync Input Clock
5
0.8 1.2 kHz
POWER SUPPLY Operating voltage range, VCC 4.75 5.0 5.25 V
Power Supply Current Low power mode 24 mA
Normal mode 49 mA
Sleep mode 500 µA
1 The digital I/O signals are driven by an internal 3.3 V supply, and the inputs are 5 V tolerant.
2 Endurance is qualified as per JEDEC Standard 22, Method A117, and measured at −40°C, +25°C, +85°C, and +125°C.
3 The data retention lifetime equivalent is at a junction temperature (TJ) of 85°C as per JEDEC Standard 22, Method A117. Data retention lifetime decreases with junction
temperature.
4 These times do not include thermal settling and internal filter response times (330 Hz bandwidth), which may affect overall accuracy.
5 The sync input clock functions below the specified minimum value, at reduced performance levels.
Data Sheet ADIS16360/ADIS16365
Rev. E | Page 5 of 20
TIMING SPECIFICATIONS
TA = 25°C, VCC = 5 V, unless otherwise noted.
Table 2.
Normal Mode
(SMPL_PRD ≤ 0x09)
Low Power Mode
(SMPL_PRD ≥ 0x0A) Burst Read
Parameter Description Min1 Typ Max Min1 Typ Max Min1 Typ Max Unit
f
SCLK
Serial clock 0.01 2.0 0.01 0.3 0.01 1.0 MHz
t
STALL
Stall period between data 9 75 1/f
SCLK
µs
t
READRATE
Read rate 40 100 µs
tCS Chip select to SCLK edge 48.8 48.8 48.8 ns
t
DAV
DOUT valid after SCLK edge 100 100 100 ns
t
DSU
DIN setup time before SCLK rising edge 24.4 24.4 24.4 ns
t
DHD
DIN hold time after SCLK rising edge 48.8 48.8 48.8 ns
tSCLKR, tSCLKF
SCLK rise/fall times
5
12.5
5
12.5
5
12.5
ns
t
DR
, t
DF
DOUT rise/fall times 5 12.5 5 12.5 5 12.5 ns
tSFS CS high after SCLK edge 5 5 5 ns
t
1
Input sync positive pulse width 5 5 µs
t
x
Input sync low time 100 100 µs
t
2
Input sync to data ready output 600 600 µs
t
3
Input sync period 833 833 µs
1 Guaranteed by design and characterization, but not tested in production.
TIMING DIAGRAMS
CS
SCLK
DOUT
DIN
1 2 3 4 5 6 15 16
R/W A5A6 A4 A3 A2 D2
MSB DB14
D1 LSB
DB13 DB12 DB10DB11 DB2 LSBDB1
t
CS
t
SFS
t
DAV
t
DHD
t
DSU
07570-002
Figure 2. SPI Timing and Sequence
CS
SCLK
tREADRATE
tSTALL
07570-003
Figure 3. Stall Time and Data Rate
t3
tX
t2
t1
SYNC
CLO CK ( DIO4)
DATA
READY
07570-004
Figure 4. Input Clock Timing Diagram
ADIS16360/ADIS16365 Data Sheet
Rev. E | Page 6 of 20
ABSOLUTE MAXIMUM RATINGS
Table 3.
Parameter Rating
Acceleration
Any Axis, Unpowered
2000
g
Any Axis, Powered 2000 g
VCC to GND −0.3 V to +6.0 V
Digital Input Voltage to GND −0.3 V to +5.3 V
Digital Output Voltage to GND −0.3 V to VCC + 0.3 V
Analog Input to GND −0.3 V to +3.6 V
Operating Temperature Range −40°C to +105°C
Storage Temperature Range −65°C to +125°C
1, 2
1 Extended exposure to temperatures outside the specified temperature
range of −40°C to +105°C can adversely affect the accuracy of the factory
calibration. For best accuracy, store the parts within the specified operating
range of −40°C to +105°C.
2 Although the device is capable of withstanding short-term exposure to
150°C, long-term exposure threatens internal mechanical integrity.
Stresses above those listed under Absolute Maximum Ratings
may cause permanent damage to the device. This is a stress
rating only; functional operation of the device at these or any
other conditions above those indicated in the operational
section of this specification is not implied. Exposure to absolute
maximum rating conditions for extended periods may affect
device reliability.
Table 4. Package Characteristics
Package Type θ
JA
θ
JC
Device Weight
24-Lead Module
(ML-24-2)
39.8°C/W 14.2°C/W 16 grams
ESD CAUTION
Data Sheet ADIS16360/ADIS16365
Rev. E | Page 7 of 20
PIN CONFIGURATION AND FUNCTION DESCRIPTIONS
NOTES
1. THIS REPRESENTATION DISPLAYS THE TOP VIEW PI NOUT
FO R THE MATING SO CKE T CONNECT OR.
2. T HE ACTUAL CONNE CTOR PI NS ARE NOT VI S IBLE F ROM
THE TOP VIEW .
3. MATING CONNECTO R: S AM TEC CLM- 112- 02
OR EQUIVALENT.
4. DNC = DO NOT CONNECT.
1
DIO3
SCLK
DIN
DIO1
DIO2
VCC
GND
GND
DNC
DNC
AUX_ADC
DNC
DIO4/CLKIN
DOUT
CS
RST
VCC
VCC
GND
DNC
DNC
AUX_DAC
DNC
DNC
2
3
4
5
6
7
8
9
10
11
12
13
14
15
16
17
18
19
20
21
22
23
24
ADIS16360/ADIS16365
TOP VIEW
(Not t o Scale)
07570-005
Figure 5. Pin Configuration
Y-AXIS
a
Y
g
Y
g
X
PIN 1
PIN 23
X-AXIS
a
X
Z-AXIS
a
Z
g
Z
ORIGIN ALIGNMENT REFERENCE POINT
SEE MSC_CTRL[6].
NOTES
1. ACCELERATI ON (
a
X
,
a
Y
,
a
Z
) AND ROTATIONAL (
g
X
,
g
Y
,
g
Z
) ARROWS
INDICATE THE DIRECTION OF MOTION THAT PRODUCES
A POSITIVE OUTPUT.
07570-006
Figure 6. Axial Orientation
Table 5. Pin Function Descriptions
Pin No. Mnemonic Type
1
Description
1
DIO3
I/O
Configurable Digital Input/Output.
2 DIO4/CLKIN I/O Configurable Digital Input/Output or Sync Clock Input.
3 SCLK I SPI Serial Clock.
4 DOUT O SPI Data Output. Clocks output on SCLK falling edge.
5 DIN I SPI Data Input. Clocks input on SCLK rising edge.
6
CS
I
SPI Chip Select.
7, 9 DIO1, DIO2 I/O Configurable Digital Input/Output.
8 RST I Reset.
10, 11, 12 VCC S Power Supply.
13, 14, 15 GND S Power Ground.
16, 17, 18, 19, 22, 23, 24
DNC
N/A
Do Not Connect.
20 AUX_DAC O Auxiliary, 12-Bit DAC Output.
21 AUX_ADC I Auxiliary, 12-Bit ADC Input.
1 I/O is input/output, I is input, O is output, S is supply, N/A is not applicable.
ADIS16360/ADIS16365 Data Sheet
Rev. E | Page 8 of 20
TYPICAL PERFORMANCE CHARACTERISTICS
0.001
0.01
0.1
0.1 110 100 1k 10k
Tau (Seconds)
ROOT ALLAN VARIANCE (°/sec)
–1σ
MEAN
+1σ
07570-007
Figure 7. Gyroscope Allan Variance
0.0001
0.001
0.01
0.1110 100 1k 10k
Tau (Seconds)
ROOT ALLAN VARIANCE (g)
–1σ
MEAN
+1σ
07570-008
Figure 8. Accelerometer Allan Variance
Data Sheet ADIS16360/ADIS16365
Rev. E | Page 9 of 20
THEORY OF OPERATION
BASIC OPERATION
The ADIS16360/ADIS16365 are autonomous sensor systems
that start up after they have a valid power supply voltage and
begin producing inertial measurement data at the factory default
sample rate setting of 819.2 SPS. After each sample cycle, the
sensor data is loaded into the output registers, and DIO1 pulses
high, which provides a new data ready control signal for driving
system-level interrupt service routines. In a typical system, a
master processor accesses the output data registers through the
SPI interface, using the connection diagram shown in Figure 9.
Table 6 provides a generic functional description for each pin on
the master processor. Table 7 describes the typical master processor
settings that are normally found in a configuration register and
used for communicating with the ADIS16360/ADIS16365.
SYSTEM
PROCESSOR
SPI MASTER
ADIS16360/
ADIS16365
SPI SLAVE
SCLK
CS
DIN
DOUT
SCLK
SS
MOSI
MISO
5V
IRQ DIO1
VDD I/O LINES ARE COMPATIBLE WITH
3.3V OR 5V LOGIC LEVELS
10
6
3
5
4
7
11 12
13 14 15
07570-009
Figure 9. Electrical Connection Diagram
Table 6. Generic Master Processor Pin Names and Functions
Pin Name
Function
SS Slave select
SCLK Serial clock
MOSI Master output, slave input
MISO Master input, slave output
IRQ Interrupt request
Table 7. Generic Master Processor SPI Settings
Processor Setting Description
Master The ADIS16360/ADIS16365 operate as slaves
SCLK Rate ≤ 2 MHz1 Normal mode, SMPL_PRD[7:0] ≤ 0x09
SPI Mode 3 CPOL = 1 (polarity), CPHA = 1 (phase)
MSB First Mode Bit sequence
16-Bit Mode Shift register/data length
1 For burst read, SCLK rate ≤ 1 MHz. For low power mode, SCLK rate ≤ 300 kHz.
The user registers provide addressing for all input/output
operations on the SPI interface. Each 16-bit register has two
7-bit addresses: one for its upper byte and one for its lower
byte. Table 8 lists the lower byte address for each register, and
Figure 10 shows the generic bit assignments.
UPPER BYTE
15 14 13 12 11 10 9 8 7 6 5 4 3 2 1 0
LOWER BYTE
07570-010
Figure 10. Generic Register Bit Assignments
READING SENSOR DATA
Although the ADIS16360/ADIS16365 produce data indepen-
dently, they operate as SPI slave devices that communicate with
system (master) processors using the 16-bit segments displayed
in Figure 11. Individual register reads require two of these 16-bit
sequences. The first 16-bit sequence contains the read command
bit (R/W = 0) and the target register address (A6 to A0); the last
eight bits are “don’t care” bits when requesting a read. The second
16-bit sequence transmits the register contents (D15 to D0) on
the DOUT line. For example, if DIN = 0x0A00, the contents of
the XACCL_OUT register are shifted out on the DOUT line
during the next 16-bit sequence.
The SPI operates in full-duplex mode, which means that the
master processor can read the output data from DOUT while
using the same SCLK pulses to transmit the next target address
on DIN.
DEVICE CONFIGURATION
The user register memory map (see Table 8) identifies configu-
ration registers with either a W or R/W. Configuration commands
also use the bit sequence shown in Figure 11. If the MSB = 1, the
last eight bits (DC7 to DC0) in the DIN sequence are loaded into
the memory address associated with the address bits (A6 to A0).
For example, if DIN = 0xA11F, 0x1F is loaded into Address 0x21
(XACCL_OFF, upper byte) at the conclusion of the data frame.
The master processor initiates the backup function by setting
GLOB_CMD[3] = 1 (DIN = 0xBE08). This command copies
the user registers into their assigned flash memory locations
and requires the power supply to stay within its normal operating
range for the entire 50 ms process. The FLASH_CNT register
provides a running count of these events for monitoring the
long-term reliability of the flash memory.
R/W R/W
A6 A5 A4 A3 A2 A1 A0 DC7 DC6 DC5 DC4 DC3 DC2 DC1 DC0
D0D1D2D3D4D5D6D7D8D9D10D11D12D13D14D15
CS
SCLK
DIN
DOUT
A6 A5
D13D14D15
NOTES
1. THE DOUT BIT PATTERN REFLECTS THE ENTIRE CONTENTS OF THE REGISTER IDENTIFIED BY [A6:A0]
IN T HE P RE V IOUS 16- BIT DIN S E QUENCE WHE N R/W = 0.
2. I F R/W = 1 DURING THE P RE V IOUS SE QUENCE, DOUT IS NOT DEF INED.
07570-011
Figure 11. SPI Communication Bit Sequence
ADIS16360/ADIS16365 Data Sheet
Rev. E | Page 10 of 20
MEMORY MAP
Table 8. User Register Memory Map
Name User Access Flash Backup Address
1
Default Register Description Bit Function
FLASH_CNT
Read only
Yes
0x00
N/A
Flash memory write count
N/A
SUPPLY_OUT Read only No 0x02 N/A Power supply measurement See Table 9
XGYRO_OUT Read only No 0x04 N/A X-axis gyroscope output See Table 9
YGYRO_OUT Read only No 0x06 N/A Y-axis gyroscope output See Table 9
ZGYRO_OUT Read only No 0x08 N/A Z-axis gyroscope output See Table 9
XACCL_OUT Read only No 0x0A N/A X-axis accelerometer output See Table 9
YACCL_OUT Read only No 0x0C N/A Y-axis accelerometer output See Table 9
ZACCL_OUT Read only No 0x0E N/A Z-axis accelerometer output See Table 9
XTEMP_OUT Read only No 0x10 N/A X-axis gyroscope temperature output See Table 9
YTEMP_OUT Read only No 0x12 N/A Y-axis gyroscope temperature output See Table 9
ZTEMP_OUT Read only No 0x14 N/A Z-axis gyroscope temperature output See Table 9
AUX_ADC Read only No 0x16 N/A Auxiliary ADC output See Table 9
Reserved N/A N/A 0x18 N/A Reserved N/A
XGYRO_OFF Read/write Yes 0x1A 0x0000 X-axis gyroscope bias offset factor See Table 15
YGYRO_OFF Read/write Yes 0x1C 0x0000 Y-axis gyroscope bias offset factor See Table 15
ZGYRO_OFF Read/write Yes 0x1E 0x0000 Z-axis gyroscope bias offset factor See Table 15
XACCL_OFF Read/write Yes 0x20 0x0000 X-axis acceleration bias offset factor See Table 16
YACCL_OFF
Read/write
Yes
0x22
0x0000
Y-axis acceleration bias offset factor
See Table 16
ZACCL_OFF Read/write Yes 0x24 0x0000 Z-axis acceleration bias offset factor See Table 16
ALM_MAG1 Read/write Yes 0x26 0x0000 Alarm 1 amplitude threshold See Table 27
ALM_MAG2 Read/write Yes 0x28 0x0000 Alarm 2 amplitude threshold See Table 27
ALM_SMPL1 Read/write Yes 0x2A 0x0000 Alarm 1 sample size See Table 28
ALM_SMPL2
Read/write
Yes
0x2C
0x0000
Alarm 2 sample size
See Table 28
ALM_CTRL Read/write Yes 0x2E 0x0000 Alarm control See Table 29
AUX_DAC Read/write No 0x30 0x0000 Auxiliary DAC data See Table 23
GPIO_CTRL Read/write No 0x32 0x0000 Auxiliary digital input/output control See Table 21
MSC_CTRL Read/write Yes 0x34 0x0006 Data ready, self-test, miscellaneous See Table 22
SMPL_PRD Read/write Yes 0x36 0x0001 Internal sample period (rate) control See Table 18
SENS_AVG Read/write Yes 0x38 0x0402 Dynamic range and digital filter control See Table 20
SLP_CNT Write only No 0x3A 0x0000 Sleep mode control See Table 19
DIAG_STAT Read only No 0x3C 0x0000 System status See Table 26
GLOB_CMD Write only No 0x3E 0x0000 System commands See Table 17
Reserved N/A N/A 0x40 to 0x51 N/A Reserved N/A
LOT_ID1 Read only Yes 0x52 N/A Lot Identification Code 1 See Table 32
LOT_ID2 Read only Yes 0x54 N/A Lot Identification Code 2 See Table 32
PROD_ID Read only Yes 0x56 0x3FE8 Product identification, ADIS16360 See Table 32
PROD_ID Read only Yes 0x56 0x3FED Product identification, ADIS16365 See Table 32
SERIAL_NUM Read only Yes 0x58 N/A Serial number See Table 32
1 Each register contains two bytes. The address of the lower byte is displayed. The address of the upper byte is equal to the address of the lower byte plus 1.
Data Sheet ADIS16360/ADIS16365
Rev. E | Page 11 of 20
BURST READ DATA COLLECTION
Burst read data collection is a process-efficient method for
collecting data from the ADIS16360/ADIS16365. In a burst
read, all output data registers are clocked out on DOUT, 16 bits
at a time, in sequential data cycles (each separated by one SCLK
period). To start a burst read sequence, set DIN = 0x3E00. The
contents of each output data register are then shifted out on
DOUT, starting with SUPPLY_OUT and ending with AUX_ADC
(see Figure 13) in order by address (see Table 8).
OUTPUT DATA REGISTERS
Each output data register uses the format in Figure 12 and Table 9.
Figure 6 shows the positive direction for each inertial sensor. The
ND bit is equal to 1 when the register contains unread data. The
EA bit is high when any error/alarm flag in the DIAG_STAT
register is equal to 1.
MSB F OR 14-BIT OUTPUT
MSB F OR 12-BIT OUTPUT
ND EA
07570-012
Figure 12. Output Data Register Bit Assignments
Table 9. Output Data Register Formats
Register Bits Scale Reference
SUPPLY_OUT 12 2.418 mV See Table 10
XGYRO_OUT1 14 0.05°/sec See Table 11
YGYRO_OUT1 14 0.05°/sec See Table 11
ZGYRO_OUT1 14 0.05°/sec See Table 11
XACCL_OUT 14 3.333 mg See Table 12
YACCL_OUT 14 3.333 mg See Table 12
ZACCL_OUT 14 3.333 mg See Table 12
XTEMP_OUT2 12 0.136°C See Table 13
YTEMP_OUT2 12 0.136°C See Table 13
ZTEMP_OUT2 12 0.136°C See Table 13
AUX_ADC 12 805.8 µV See Table 14
1 Assumes that the scaling is set to ±300°/sec. This factor scales with the range.
2 0x0000 = 25°C (±5°C).
Table 10. Power Supply, Offset Binary Format
Supply Voltage Decimal Hex Binary
5.25 V 2171 LSB 0x87B XXXX 1000 0111 1011
5.002418 V 2069 LSB 0x815 XXXX 1000 0001 0101
5 V 2068 LSB 0x814 XXXX 1000 0001 0100
4.997582 V 2067 LSB 0x813 XXXX 1000 0001 0011
4.75 V 1964 LSB 0x7AC XXXX 0111 1010 1100
Table 11. Rotation Rate, Twos Complement Format
Rotation Rate Decimal Hex Binary
+300°/sec +6000 LSB 0x1770 XX01 0111 0111 0000
+0.1°/sec +2 LSB 0x0002 XX00 0000 0000 0010
+0.05°/sec +1 LSB 0x0001 XX00 0000 0000 0001
0°/sec 0 LSB 0x0000 XX00 0000 0000 0000
−0.05°/sec −1 LSB 0x3FFF XX11 1111 1111 1111
−0.1°/sec −2 LSB 0x3FFE XX11 1111 1111 1110
−300°/sec −6000 LSB 0x2890 XX10 1000 1001 0000
Table 12. Acceleration, Twos Complement Format
Acceleration Decimal Hex Binary
+18 g +5401 LSB 0x1519 XX01 0101 0001 1001
+6.667 mg +2 LSB 0x0002 XX00 0000 0000 0010
+3.333 mg +1 LSB 0x0001 XX00 0000 0000 0001
0 g 0 LSB 0x0000 XX00 0000 0000 0000
−3.333 mg −1 LSB 0x3FFF XX11 1111 1111 1111
−6.667 mg −2 LSB 0x3FFE XX11 1111 1111 1110
−18 g −5401 LSB 0x2AE7 XX10 1010 1110 0111
Table 13. Temperature, Twos Complement Format
Temperature Decimal Hex Binary
+105°C +588 LSB 0x24C XXXX 0010 0100 1100
+85°C +441 LSB 0x1B9 XXXX 0001 1011 1001
+25.272°C +2 LSB 0x002 XXXX 0000 0000 0010
+25.136°C +1 LSB 0x001 XXXX 0000 0000 0001
+25°C 0 LSB 0x000 XXXX 0000 0000 0000
+24.864°C −1 LSB 0xFFF XXXX 1111 1111 1111
+24.728°C
−2 LSB
0xFFE
XXXX 1111 1111 1110
−40°C −478 LSB 0xE22 XXXX 1110 0010 0010
Table 14. Analog Input, Offset Binary Format
Input Voltage Decimal Hex Binary
3.3 V 4095 LSB 0xFFF XXXX 1111 1111 1111
1 V 1241 LSB 0x4D9 XXXX 0100 1101 1001
1.6116 mV 2 LSB 0x002 XXXX 0000 0000 0010
805.8 µV 1 LSB 0x001 XXXX 0000 0000 0001
0 V 0 LSB 0x000 XXXX 0000 0000 0000
0x3E00
PREVIOUS
DON’ T CARE
SUPPLY_OUT XGYRO_OUT AUX_ADC
123 12
YGYRO_OUT ZGYRO_OUT
4 5CS
SCLK
DIN
DOUT
NOTES
1. T HE DOUT LINE HAS BEEN S IMPLIFIE D FOR SPACE CONSTRAI NTS BUT, IDEALLY , SHOUL D INCLUDE AL L REGI S TERS FROM SUPPLY_OUT THROUGH AUX _ADC.
07570-013
Figure 13. Burst Read Sequence
ADIS16360/ADIS16365 Data Sheet
Rev. E | Page 12 of 20
CALIBRATION
Manual Bias Calibration
The bias offset registers in Table 15 and Table 16 provide a
manual adjustment function for the output of each sensor. For
example, if XGYRO_OFF = 0x1FF6 (DIN = 0x9B1F, 0x9AF6),
the XGYRO_OUT offset shifts by −10 LSBs, or −0.125°/sec.
Table 15. XGYRO_OFF, YGYRO_OFF, ZGYRO_OFF
Bit Descriptions
Bits Description (Default = 0x0000)
[15:13] Not used.
[12:0] Data bits. Twos complement, 0.0125°/sec per LSB.
Typical adjustment range = ±50°/sec.
Table 16. XACCL_OFF, YACCL_OFF, ZACCL_OFF
Bit Descriptions
Bits Description (Default = 0x0000)
[15:12] Not used.
[11:0] Data bits. Twos complement, 3.333 mg/LSB.
Typical adjustment range = ±6.7 g.
Gyroscope Automatic Bias Null Calibration
Set GLOB_CMD[0] = 1 (DIN = 0xBE01) to execute the auto-
matic bias null calibration function. This function measures all
three gyroscope output registers and then loads each gyroscope
offset register with the opposite value to provide a quick bias
calibration. All sensor data is then reset to 0, and the flash
memory is updated automatically within 50 ms (see Table 17).
Gyroscope Precision Automatic Bias Null Calibration
Set GLOB_CMD[4] = 1 (DIN = 0xBE10) to execute the precision
automatic bias null calibration function. This function takes the
sensor offline for 30 sec while it collects a set of data and calculates
more accurate bias correction factors for each gyroscope. After
this function is executed, the newly calculated correction factor
is loaded into the gyroscope offset registers, all sensor data is
reset to 0, and the flash memory is updated automatically within
50 ms (see Table 17).
Restoring Factory Calibration
Set GLOB_CMD[1] = 1 (DIN = 0xBE02) to execute the factory
calibration restore function. This function resets each user cali-
bration register to 0x0000 (see Table 15 and Table 16), resets all
sensor data to 0, and automatically updates the flash memory
within 50 ms (see Table 17).
Linear Acceleration Bias Compensation (Gyroscope)
Set MSC_CTRL[7] = 1 (DIN = 0xB486) to enable correction for
low frequency acceleration influences on gyroscope bias. The
DIN sequence also preserves the factory default condition for
the data ready function (see Table 22).
OPERATIONAL CONTROL
Global Commands
The GLOB_CMD register provides trigger bits for several use-
ful functions. Setting the assigned bit to 1 starts each operation,
which returns the bit to 0 after completion. For example, set
GLOB_CMD[7] = 1 (DIN = 0xBE80) to execute a software reset,
which stops the sensor operation and runs the device through
its start-up sequence. This sequence includes loading the control
registers with the data in their respective flash memory locations
prior to producing new data. Reading the GLOB_CMD register
(DIN = 0x3E00) starts the burst read sequence.
Table 17. GLOB_CMD Bit Descriptions
Bits Description (Default = 0x0000)
[15:8] Not used
[7] Software reset command
[6:5] Not used
[4] Precision autonull command
[3] Flash update command (see the Device Configuration
section)
[2] Auxiliary DAC data latch (see the Auxiliary DAC section)
[1] Factory calibration restore command
[0]
Autonull command
Internal Sample Rate
The SMPL_PRD register provides discrete sample period settings
using the bit assignments in Tabl e 18 and the following equation:
tS = tB × (NS + 1)
To calculate the internal sample rate, divide 1 by the sample
period (tS). For example, when SMPL_PRD[7:0] = 0x0A, the
sample rate is 149 SPS.
Table 18. SMPL_PRD Bit Descriptions
Bits Description (Default = 0x0001)
[15:8] Not used
[7] Time base (t
B
)
0 = 0.61035 ms, 1 = 18.921 ms
[6:0] Increment setting (N
S
)
Internal sample period = tS = tB × (NS + 1)
The default sample rate setting of 819.2 SPS preserves the sensor
bandwidth and provides optimal performance. For systems that
value slower sample rates, keep the internal sample rate at
819.2 SPS. Use the programmable filter (SENS_AVG) to reduce
the bandwidth, which helps to prevent aliasing. The data ready
function (MSC_CTRL) can drive an interrupt routine that uses
a counter to help ensure data coherence at the reduced rates.
Data Sheet ADIS16360/ADIS16365
Rev. E | Page 13 of 20
Power Management
Setting SMPL_PRD ≥ 0x0A also sets the sensor to low power
mode. For systems that require lower power dissipation, in-
system characterization helps users to quantify the associated
performance trade-offs. In addition to sensor performance, this
mode affects SPI data rates (see Table 2). Set SLP_CNT[8] = 1
(DIN = 0xBB01) to start the indefinite sleep mode, which requires
a CS assertion (high to low), reset, or power cycle to wake up.
Use SLP_CNT[7:0] to put the device into sleep mode for a
specified period. For example, SLP_CNT[7:0] = 0x64 (DIN =
0xBA64) puts the ADIS16360/ADIS16365 to sleep for 50 sec.
Table 19. SLP_CNT Bit Descriptions
Bits Description (Default = 0x0000)
[15:9] Not used
[8] Indefinite sleep mode; set to 1
[7:0] Programmable sleep time bits, 0.5 sec/LSB
Sensor Bandwidth
The signal chain for each MEMS sensor has several filter stages,
which shape their frequency response. Figure 14 provides a
block diagram for both gyroscope and accelerometer signal
paths. Table 20 provides additional information for digital filter
configuration.
LPF LPF NN
404Hz
FROM
GYROSCOPE
SENSOR 757Hz
LPF NN
FROM
ACCELERATION
SENSOR 330Hz N = 2m
m = SENS _AV G[2:0]
07570-114
Figure 14. MEMS Analog and Digital Filters
Digital Filtering
The N blocks in Figure 14 are part of the programmable low-pass
filter, which provides additional noise reduction on the inertial
sensor outputs. This filter contains two cascaded averaging filters
that provide a Bartlett window, FIR filter response (see Figure 15).
For example, set SENS_AVG[2:0] = 100 (DIN = 0xB804) to set
each stage to 16 taps. When used with the default sample rate of
819.2 SPS, this value reduces the sensor bandwidth to approxi-
mately 16 Hz.
0
–20
–40
–60
–80
–100
–120
–140
0.001 0.01 0.1 1
MAG NITUDE (dB)
FRE QUENCY (
f
/
fS
)
N = 2
N = 4
N = 16
N = 64
07570-014
Figure 15. Bartlett Window, FIR Filter Frequency Response
(Phase Delay = N Samples)
Dynamic Range
The SENS_AVG[10:8] bits provide three dynamic range settings
for this gyroscope. The lower dynamic range settings (±75°/sec
and ±150°/sec) limit the minimum filter tap sizes to maintain
resolution. For example, set SENS_AVG[10:8] = 010 (DIN =
0xB902) for a measurement range of ±150°/sec. Because this
setting can influence the filter settings, program SENS_AVG[10:8]
and then SENS_AVG[2:0] if more filtering is required.
Table 20. SENS_AVG Bit Descriptions
Bits Description (Default = 0x0402)
[15:11] Not used
[10:8] Measurement range (sensitivity) selection
100 = ±300°/sec (default condition)
010 = ±150°/sec, filter taps ≥ 4 (Bits[2:0] ≥ 0x02)
001 = ±75°/sec, filter taps ≥ 16 (Bits[2:0] ≥ 0x04)
[7:3]
Not used
[2:0] Number of taps in each stage; value of m in N = 2
m
ADIS16360/ADIS16365 Data Sheet
Rev. E | Page 14 of 20
INPUT/OUTPUT FUNCTIONS
General-Purpose I/O
DIO1, DIO2, DIO3, and DIO4 are configurable, general-purpose
I/O lines that serve multiple purposes according to the follow-
ing control register priority: MSC_CTRL, ALM_CTRL, and
GPIO_CTRL. For example, set GPIO_CTRL = 0x080C (DIN =
0xB308, and then 0xB20C) to configure DIO1 and DIO2 as
inputs and DIO3 and DIO4 as outputs, with DIO3 set low and
DIO4 set high.
In this configuration, read GPIO_CTRL (DIN = 0x3200). The
digital state of DIO1 and DIO2 is in GPIO_CTRL[9:8].
Table 21. GPIO_CTRL Bit Descriptions
Bits Description (Default = 0x0000)
[15:12] Not used
[11] General-Purpose I/O Line 4 (DIO4) data level
[10] General-Purpose I/O Line 3 (DIO3) data level
[9] General-Purpose I/O Line 2 (DIO2) data level
[8] General-Purpose I/O Line 1 (DIO1) data level
[7:4] Not used
[3] General-Purpose I/O Line 4 (DIO4) direction control
(1 = output, 0 = input)
[2]
General-Purpose I/O Line 3 (DIO3) direction control
(1 = output, 0 = input)
[1] General-Purpose I/O Line 2 (DIO2) direction control
(1 = output, 0 = input)
[0] General-Purpose I/O Line 1 (DIO1) direction control
(1 = output, 0 = input)
Input Clock Configuration
The input clock function allows for external control of sampling
in the ADIS16360/ADIS16365. Set GPIO_CTRL[3] = 0 (DIN =
0xB200) and SMPL_PRD[7:0] = 0x00 (DIN = 0xB600) to enable
this function. See Table 2 and Figure 4 for timing information.
Data Ready I/O Indicator
The factory default sets DIO1 as a positive data ready indicator
signal. The MSC_CTRL[2:0] bits provide configuration options
for changing the default. For example, set MSC_CTRL[2:0] =
100 (DIN = 0xB404) to change the polarity of the data ready
signal on DIO1 for interrupt inputs that require negative logic
inputs for activation. The pulse width is between 100 µs and
200 µs over all conditions.
Table 22. MSC_CTRL Bit Descriptions
Bits Description (Default = 0x0006)
[15:12] Not used
[11] Memory test (cleared upon completion)
(1 = enabled, 0 = disabled)
[10] Internal self-test enable (cleared upon completion)
(1 = enabled, 0 = disabled)
[9] Manual self-test, negative stimulus
(1 = enabled, 0 = disabled)
[8] Manual self-test, positive stimulus
(1 = enabled, 0 = disabled)
[7]
Linear acceleration bias compensation for gyroscopes
(1 = enabled, 0 = disabled)
[6] Linear accelerometer origin alignment
(1 = enabled, 0 = disabled)
[5:3] Not used
[2] Data ready enable
(1 = enabled, 0 = disabled)
[1] Data ready polarity
(1 = active high, 0 = active low)
[0] Data ready line select
(1 = DIO2, 0 = DIO1)
Auxiliary DAC
The 12-bit AUX_DAC line can drive its output to within 5 mV
of the ground reference when it is not sinking current. As the
output approaches 0 V, the linearity begins to degrade (~100 LSB
starting point). As the sink current increases, the nonlinear range
increases. The DAC latch command moves the values of the
AUX_DAC register into the DAC input register, enabling both
bytes to take effect at the same time.
Table 23. AUX_DAC Bit Descriptions
Bits Description (Default = 0x0000)
[15:12] Not used
[11:0] Data bits, scale factor = 0.8059 mV/LSB
Offset binary format, 0 V = 0 LSB
Table 24. Setting AUX_DAC = 1 V
DIN Description
0xB0D9 AUX_DAC[7:0] = 0xD9 (217 LSB).
0xB104 AUX_DAC[15:8] = 0x04 (1024 LSB).
0xBE04
GLOB_CMD[2] = 1.
Move values into the DAC input register, resulting in
a 1 V output level.
Data Sheet ADIS16360/ADIS16365
Rev. E | Page 15 of 20
DIAGNOSTICS
Self-Test
The self-test function allows the user to verify the mechanical
integrity of each MEMS sensor. It applies an electrostatic force
to each sensor element, which results in mechanical displace-
ment that simulates a response to actual motion. Table 1 lists
the expected response for each sensor and provides pass/fail
criteria.
Set MSC_CTRL[10] = 1 (DIN = 0xB504) to run the internal
self-test routine, which exercises all inertial sensors, measures
each response, makes pass/fail decisions, and reports them to
error flags in the DIAG_STAT register. MSC_CTRL[10] resets
itself to 0 after completing the routine. The MSC_CTRL[9:8] bits
provide manual control over the self-test function for investiga-
tion of potential failures. Table 25 outlines an example test flow
for using this option to verify the x-axis gyroscope function.
Table 25. Manual Self-Test Example Sequence
DIN Description
0xB601 SMPL_PRD[7:0] = 0x01, sample rate = 819.2 SPS.
0xB904 SENS_AVG[15:8] = 0x04, gyro range = ±300°/sec.
0xB802 SENS_AVG[7:0] = 0x02, four-tap averaging filter.
Delay = 50 ms.
0x0400
Read XGYRO_OUT.
0xB502 MSC_CTRL[9:8] = 10, gyroscope negative self-test.
Delay = 50 ms.
0x0400 Read XGYRO_OUT.
Determine whether the bias in the gyroscope
output changed according to the self-test response
specified in Table 1.
0xB501 MSC_CTRL[9:8] = 01, gyroscope/accelerometer
positive self-test.
Delay = 50 ms.
0x0400 Read XGYRO_OUT.
Determine whether the bias in the gyroscope
output changed according to the self-test response
specified in Table 1.
0xB500 MSC_CTRL[15:8] = 0x00.
Zero motion provides results that are more reliable. The set-
tings in Table 25 are flexible and allow for optimization around
speed and noise influence. For example, using fewer filtering
taps decreases delay times but increases the possibility of noise
influence.
Memory Test
Setting MSC_CTRL[11] = 1 (DIN = 0xB508) performs a check-
sum verification of the flash memory locations. The pass/fail
result is loaded into DIAG_STAT[6].
Status
The error flags provide indicator functions for common
system level issues. All of the flags are cleared (set to 0) after
each DIAG_STAT register read cycle. If an error condition
remains, the error flag returns to 1 during the next sample
cycle. The DIAG_STAT[1:0] bits do not require a read of this
register to return to 0. If the power supply voltage goes back
into range, these two flags are cleared automatically.
Table 26. DIAG_STAT Bit Descriptions
Bits Description (Default = 0x0000)
[15] Z-axis accelerometer self-test failure (1 = fail, 0 = pass)
[14] Y-axis accelerometer self-test failure (1 = fail, 0 = pass)
[13] X-axis accelerometer self-test failure (1 = fail, 0 = pass)
[12] Z-axis gyroscope self-test failure (1 = fail, 0 = pass)
[11] Y-axis gyroscope self-test failure (1 = fail, 0 = pass)
[10] X-axis gyroscope self-test failure (1 = fail, 0 = pass)
[9] Alarm 2 status (1 = active, 0 = inactive)
[8] Alarm 1 status (1 = active, 0 = inactive)
[7] Not used
[6] Flash test, checksum flag (1 = fail, 0 = pass)
[5] Self-test diagnostic error flag (1 = fail, 0 = pass)
[4] Sensor overrange (1 = fail, 0 = pass)
[3] SPI communication failure (1 = fail, 0 = pass)
[2]
Flash update failure (1 = fail, 0 = pass)
[1] Power supply > 5.25 V
1 = power supply > 5.25 V, 0 = power supply ≤ 5.25 V
[0] Power supply < 4.75 V
1 = power supply < 4.75 V, 0 = power supply ≥ 4.75 V
Alarm Registers
The alarm function provides monitoring for two independent
conditions. The ALM_CTRL register provides control inputs
for data source, data filtering (prior to comparison), static
comparison, dynamic rate-of-change comparison, and output
indicator configurations. The ALM_MAGx registers establish
the trigger threshold and polarity configurations. Table 30 gives
an example of how to configure a static alarm. The ALM_SMPLx
registers provide the numbers of samples to use in the dynamic
rate-of-change configuration. The period equals the number in
the ALM_SMPLx register multiplied by the sample period time,
which is established by the SMPL_PRD register. See Table 31 for
an example of how to configure the sensor for this type of function.
ADIS16360/ADIS16365 Data Sheet
Rev. E | Page 16 of 20
Table 27. ALM_MAG1, ALM_MAG2 Bit Descriptions
Bits Description (Default = 0x0000)
[15] Comparison polarity
(1 = greater than, 0 = less than)
[14] Not used
[13:0] Data bits that match the format of the trigger source
selection
Table 28. ALM_SMPL1, ALM_SMPL2 Bit Descriptions
Bits Description (Default = 0x0000)
[15:8] Not used
[7:0] Data bits: number of samples (both 0x00 and 0x01 = 1)
Table 29. ALM_CTRL Bit Descriptions
Bits Description (Default = 0x0000)
[15:12] Alarm 2 source selection
0000 = disable
0001 = power supply output
0010 = x-axis gyroscope output
0011 = y-axis gyroscope output
0100 = z-axis gyroscope output
0101 = x-axis accelerometer output
0110 = y-axis accelerometer output
0111 = z-axis accelerometer output
1000 = x-axis gyroscope temperature output
1001 = y-axis gyroscope temperature output
1010 = z-axis gyroscope temperature output
1011 = auxiliary ADC input
[11:8] Alarm 1 source selection (same as Alarm 2)
[7] Rate-of-change enable for Alarm 2
(1 = rate of change, 0 = static level)
[6] Rate-of-change enable for Alarm 1
(1 = rate of change, 0 = static level)
[5] Not used
[4] Comparison data filter setting
(1 = filtered data, 0 = unfiltered data)
[3] Not used
[2] Alarm output enable
(1 = enabled, 0 = disabled)
[1] Alarm output polarity
(1 = active high, 0 = active low)
[0] Alarm output line select
(1 = DIO2, 0 = DIO1)
Table 30. Alarm Configuration Example 1
DIN Description
0xAF55,
0xAE17
ALM_CTRL = 0x5517.
Alarm 1 input = XACCL_OUT.
Alarm 2 input = XACCL_OUT.
Static level comparison, filtered data.
DIO2 output indicator, positive polarity.
0xA700,
0xA696
ALM_MAG1 = 0x8096.
Alarm 1 is true if XACCL_OUT > +0.5 g.
0xA937,
0xA86A
ALM_MAG2 = 0x376A.
Alarm 2 is true if XACCL_OUT < −0.5 g.
Table 31. Alarm Configuration Example 2
DIN Description
0xAF76,
0xAEC7
ALM_CTRL = 0x76C7.
Alarm 1 input = YACCL_OUT.
Alarm 2 input = ZACCL_OUT.
Rate-of-change comparison, unfiltered data.
DIO2 output indicator, positive polarity.
0xB601 SMPL_PRD = 0x0001.
Sample rate = 819.2 SPS.
0xAA08 ALM_SMPL1 = 0x0008.
Alarm 1 rate-of-change period = 9.77 ms.
0xAC50 ALM_SMPL2 = 0x0050.
Alarm 2 rate-of-change period = 97.7 ms.
0xA700,
0xA696
ALM_MAG1 = 0x8096.
Alarm 1 is true if YACCL_OUT increases by more than
0.5 g in 9.77 ms.
0xA937,
0xA86A
ALM_MAG2 = 0x376A.
Alarm 2 is true if ZACCL_OUT decreases by more
than 0.5 g in 97.7 ms.
PRODUCT IDENTIFICATION
Table 32 provides a summary of the registers that identify
the product: PROD_ID, which identifies the product type;
LOT_ID1 and LOT_ID2, the 32-bit lot identification code;
and SERIAL_NUM, which displays the 12-bit serial number.
All four registers are two bytes in length. When using the
SERIAL_NUM value to calculate the serial number, mask
off the upper four bits and convert the remaining 12 bits to
a decimal number.
Table 32. Identification Registers
Register Name Address Description
LOT_ID1 0x52 Lot Identification Code 1
LOT_ID2 0x54 Lot Identification Code 2
PROD_ID 0x56 Product identification:
0x3FE8 (16,360)
0x3FED (16,365)
SERIAL_NUM
0x58
Serial number
Data Sheet ADIS16360/ADIS16365
Rev. E | Page 17 of 20
APPLICATIONS INFORMATION
INSTALLATION/HANDLING
For ADIS16360/ADIS16365 installation, use the following
two-step process:
1. Secure the baseplate using machine screws.
2. Press the connector into its mate.
For removal,
1. Gently pry the connector from its mate using a small slot
screwdriver.
2. Remove the screws and lift the part up.
Never attempt to unplug the connector by pulling on the plastic
case or baseplate. Although the flexible connector is very reliable
in normal operation, it can break when subjected to unreasonable
handling. When broken, the flexible connector cannot be repaired.
The AN-1041 Application Note, iSensor® IMU Quick Start Guide
and Bias Optimization Tips, provides more information about
developing an appropriate mechanical interface design.
GYROSCOPE BIAS OPTIMIZATION
The factory calibration addresses initial bias errors along with
temperature-dependent bias behaviors. Installation and certain
environmental conditions can introduce modest bias errors.
The precision autonull command (GLOB_CMD[4]) provides a
simple predeployment method for correcting these errors to an
accuracy of approximately 0.008°/sec, using an average of 30 sec.
Averaging the sensor output data for 100 sec can provide incre-
mental performance gains, as well. Controlling device rotation,
power supply, and temperature during these averaging times
helps to ensure optimal accuracy during this process. Refer to
the AN-1041 Application Note for more information about
optimizing performance.
INPUT ADC CHANNEL
The AUX_ADC register provides access to the auxiliary ADC
input channel. The ADC is a 12-bit successive approximation
converter that has an input circuit equivalent to the one shown
in Figure 16. The maximum input is 3.3 V. The ESD protection
diodes can handle 10 mA without causing irreversible damage.
The on resistance (R1) of the switch has a typical value of 100 Ω.
The sampling capacitor, C2, has a typical value of 16 p F.
C2
C1
R1
VCC
D
D
07570-015
Figure 16. Equivalent Analog Input Circuit
(Conversion Phase: Switch Open,
Track Phase: Switch Closed)
INTERFACE PRINTED CIRCUIT BOARD (PCB)
The ADIS16360/PCBZ includes one ADIS16360BMLZ and
one interface PCB. The ADIS16365/PCBZ includes one
ADIS16365BMLZ and one interface PCB. The interface PCB
simplifies the process of integrating these products into an
existing processor system.
J1 and J2 are dual-row, 2 mm (pitch) connectors that work
with a number of ribbon cable systems, including 3M Part
Number 152212-0100-GB (ribbon crimp connector) and
3M Part Number 3625/12 (ribbon cable). Figure 17 provides
a hole pattern design for installing the ADIS16360BMLZ/
ADIS16365BMLZ and the interface PCB onto the same
surface. Figure 18 provides the pin assignments for each
connector. The pin descriptions match those listed in Table 5.
The ADIS16360/ADIS16365 do not require external capacitors
for normal operation; therefore, the interface PCB does not use
the C1/C2 pads (not shown in Figure 17).
11 12
2
1
21
11 12
J2
J1
23.75 21.24
30.10 27.70
1.20
NOTES
1. DIMENSIONS IN MILLIMETERS.
07570-016
Figure 17. Physical Diagram for the ADIS16360/PCBZ and ADIS16365/PCBZ
1 2
3 4
5 6
7 8
910
11 12
AUX_ADC
AUX_DAC
DNC
DNC
DIO2
DNC
DNC
DIO1
DIO4
DIO3
GND
J2
GND
2
4
6
8
10
1
3
5
7
9
11 12
RST
CS
GND
GND
VCC
GND
VCC
VCC
DIN
DOUT
SCLK
J1
DNC
07570-017
Figure 18. J1/J2 Pin Assignments
ADIS16360/ADIS16365 Data Sheet
Rev. E | Page 18 of 20
OUTLINE DIMENSIONS
TOP VI EW
BOTTOM VIEW
FRONT VIEW
DETAIL A
CASTING
FEATURE
SIDE VIEW
22.964
22.710
22.456
14.950
14.550
14.150
21.410
21.210
21.010
23.504
23.250
22.996
5.20
5.00
4.80
(2×)
4.20
4.00
3.80
(2×)
17.41
17.21
17.01
(2×)
2.660
2.500
2.340
23.454
23.200
22.946
31.900
31.700
31.500
4.330
BSC
1.588
BSC
2.382
BSC
PI N 24
PI N 1
9.464
9.210
8.956
(2×)
DETAIL A
14.00 BS C
0.305
BSC (24×) 1.00
BSC (22×) 1.65 BSC
4.162 BS C
7.18
BSC
1.588
BSC
12.10
BSC
0.05
BSC
1.00
BSC
2.00 BS C
10.50
BSC
10.60
BSC
12-16-2011-C
Figure 19. 24-Lead Module with Connector Interface
(ML-24-2)
Dimensions shown in millimeters
ORDERING GUIDE
Model
1
Temperature Range Package Description Package Option
ADIS16360BMLZ −40°C to +105°C 24-Lead Module with Connector Interface ML-24-2
ADIS16360/PCBZ Interface Board
ADIS16365BMLZ −40°C to +105°C 24-Lead Module with Connector Interface ML-24-2
ADIS16365/PCBZ Interface Board
1 Z = RoHS Compliant Part.
Data Sheet ADIS16360/ADIS16365
Rev. E | Page 19 of 20
NOTES
