ADIS16485BMLZ

Tactical Grade, Six Degrees of Freedom Inertial Sensor ADIS16485 Data Sheet FEATURES GENERAL DESCRIPTION Triaxial, digital gyroscope, ±450°/sec dynamic range ±0.05° orthogonal alignment error 6°/hr in-run bias stability 0.3°/√hr angular random walk 0.01% nonlinearity Triaxial, digital accelerometer, ±5 g Triaxial, delta angle, and delta velocity outputs Fast start-up time, ~500 ms Factory calibrated sensitivity, bias, and axial alignment Calibration temperature range: −40°C to +85°C SPI-compatible serial interface Embedded temperature sensor Programmable operation and control Automatic and manual bias correction controls 4 FIR filter banks, 120 configurable taps Digital I/O: data-ready alarm indicator, external clock Alarms for condition monitoring Power-down/sleep mode for power management Optional external sample clock input: up to 2.4 kHz Single command self test Single-supply operation: 3.0 V to 3.6 V 2000 g shock survivability Operating temperature range: −40°C to +105°C The ADIS16485 iSensor® device is a complete inertial system that includes a triaxial gyroscope and a triaxial accelerometer. Each inertial sensor in the ADIS16485 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 (gyroscope bias). As a result, each sensor has its own dynamic compensation formulas that provide accurate sensor measurements. The ADIS16485 provides 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 navigation systems. The SPI and register structure provide a simple interface for data collection and configuration control. The ADIS16485 uses the same footprint and connector system as the ADIS16375 and the ADIS16488A, which greatly simplifies the upgrade process. It comes in a module that is approximately 47 mm × 44 mm × 14 mm and has a standard connector interface. APPLICATIONS Platform stabilization and control Navigation Personnel tracking Instruments Robotics FUNCTIONAL BLOCK DIAGRAM DIO1 DIO2 DIO3 DIO4 RST SELF TEST I/O VDD ALARMS TRIAXIAL GYRO POWER MANAGEMENT OUTPUT DATA REGISTERS TRIAXIAL ACCEL CONTROLLER TEMP CALIBRATION AND FILTERS VDD GND CS SCLK SPI USER CONTROL REGISTERS DIN DOUT ADIS16485 VDDRTC 10666-001 CLOCK Figure 1. Rev. H Document Feedback Information furnished by Analog Devices is believed to be accurate and reliable. However, no responsibility is assumed by Analog Devices for its use, nor for any infringements of patents or other rights of third parties that may result from its use. Specifications subject to change without notice. No license is granted by implication or otherwise under any patent or patent rights of Analog Devices. Trademarks and registered trademarks are the property of their respective owners. One Technology Way, P.O. Box 9106, Norwood, MA 02062-9106, U.S.A. Tel: 781.329.4700 ©2012−2019 Analog Devices, Inc. All rights reserved. Technical Support www.analog.com ADIS16485 Data Sheet TABLE OF CONTENTS Features .............................................................................................. 1 Product Identification................................................................ 19 Applications ....................................................................................... 1 Digital Signal Processing ............................................................... 20 General Description ......................................................................... 1 Gyroscopes/Accelerometers ..................................................... 20 Functional Block Diagram .............................................................. 1 Averaging/Decimation Filter .................................................... 20 Revision History ............................................................................... 3 FIR Filter Banks .......................................................................... 21 Specifications..................................................................................... 4 Calibration ....................................................................................... 23 Timing Specifications .................................................................. 6 Gyroscopes .................................................................................. 23 Absolute Maximum Ratings............................................................ 8 Accelerometers ........................................................................... 24 ESD Caution .................................................................................. 8 Restoring Factory Calibration .................................................. 25 Pin Configuration and Function Descriptions ............................. 9 Point of Percussion Alignment ................................................. 25 Typical Performance Characteristics ........................................... 10 Alarms .............................................................................................. 26 Basic Operation............................................................................... 11 Static Alarm Use ......................................................................... 26 Register Structure ....................................................................... 11 Dynamic Alarm Use .................................................................. 26 SPI Communication ................................................................... 12 System Controls .............................................................................. 27 Device Configuration ................................................................ 12 Global Commands ..................................................................... 27 Reading Sensor Data .................................................................. 12 Memory Management ............................................................... 27 User Registers .................................................................................. 13 General-Purpose I/O ................................................................. 28 Output Data Registers .................................................................... 16 Power Management ................................................................... 28 Inertial Sensor Data Format...................................................... 16 Applications Information .............................................................. 30 Rotation Rate (Gyroscope) ........................................................ 16 Mounting Tips ............................................................................ 30 Acceleration................................................................................. 17 Evaluation Tools ......................................................................... 31 Delta Angles ................................................................................ 17 Power Supply Considerations ................................................... 31 Delta Velocity .............................................................................. 18 X-Ray Sensitivity ........................................................................ 31 Internal Temperature ................................................................. 18 Outline Dimensions ....................................................................... 32 Status/Alarm Indicators ............................................................. 19 Ordering Guide .......................................................................... 32 Firmware Revision ..................................................................... 19 Rev. H | Page 2 of 32 Data Sheet ADIS16485 REVISION HISTORY 2/2019—Rev. G to Rev. H Added Endnote 3, Table 1; Renumbered Sequentially ................. 5 Added X-Ray Sensitivity Section ..................................................31 9/2017—Rev. F to Rev. G Changed ADIS16488 to ADIS16488A ....................... Throughout Changes to Logic Inputs Parameter, Table 1 .................................. 4 Added Endnote 4, Table 1; Renumbered Sequentially ................. 5 Changed PC-Based Evaluation, EVAL-ADIS Section Title to PC-Based Evaluation, EVAL-ADIS2 Section Title .....................31 Changes to PC-Based Evaluation, EVAL-ADIS2 Section ..........31 10/2016—Rev. E to Rev. F Changes to Figure 29 ......................................................................31 2/2015—Rev. D to Rev. E Changes to Features Section ............................................................ 1 Changes to Table 1 ............................................................................ 4 Changes to Table 2 and Figure 2 ..................................................... 6 Added Table 3; Renumbered Sequentially ..................................... 6 Change to Figure 4 ............................................................................ 7 Change to Operating Temperature Range, Table 4 ....................... 8 Change to Dual Memory Structure Section ................................12 Changes to Ordering Guide ...........................................................32 5/2014—Rev. C to Rev. D Changes to Table 73, Table 74, and Table 75................................23 4/2014—Rev. B to Rev. C Change to Features Section .............................................................. 1 Moved Revision History ................................................................... 3 Added Endnote 7; Renumbered Sequentially, and Changes to Endnote 9, Table 1 ............................................................................. 5 Changes to Table 9 ..........................................................................14 Changes to Delta Angles Section ..................................................16 Changes to Delta Velocity Section ................................................17 Change to Figure 20 Caption .........................................................19 Changes to Linear Acceleration on Effect on Gyroscope Bias Section and Manual Bias Correction ............................................23 Changes to Status Alarm Use Section and Dynamic Alarm Use Section ....................................................................................... 25 Change to Software Reset Section ................................................ 26 Changes to General-Purpose I/O Section ................................... 27 12/2013—Rev. A to Rev. B Change to t2 Parameter, Table 2....................................................... 5 Change to Figure 6 ............................................................................ 7 Changes to Delta Angles Section .................................................. 15 Changes to Delta Velocity Section ................................................ 16 Changes to Status/Alarm Indicators Section ............................... 17 Deleted Prototype Interface Board Section, PC Evaluation with EVAL_ADIS Section, Mechanical Design Tips Section, Figure 26, Figure 27, Figure 30, and Figure 31; Renumbered Sequentially .....27 Added Mounting Tips Section and Figure 26; Renumbered Sequentially ...................................................................................... 27 Added Evaluation Tools Section, Power Supply Considerations Section, Figure 29 and Figure 30; Renumbered Sequentially ... 28 Changes to Ordering Guide ........................................................... 29 12/2012—Rev. 0 to Rev. A Changes to Table 1 ............................................................................ 3 Added tSFS Parameter, Table 2 .......................................................... 5 Changes to t2 Parameter, Table 2 and Figure 2 .............................. 5 Changes to Figure 8 .......................................................................... 8 Changes to Linear Acceleration on Effect on Gyroscope Bias Section .............................................................................................. 21 Changes to Prototype Interface Board Section ........................... 27 Deleted Installation Tips Section, and Figure 28; Renumbered Sequentially ...................................................................................... 27 Added Mechanical Design Tips Section, Connector Down Mounting Tips Section, and Figure 28; Renumbered Sequentially ...................................................................................... 27 Added Connector Up Mounting Tips Section, Figure 30, and Figure 31 ........................................................................................... 28 Updated Outline Dimensions........................................................ 29 5/2012—Revision 0: Initial Version Rev. H | Page 3 of 32 ADIS16485 Data Sheet SPECIFICATIONS TA = 25°C, VDD = 3.3 V, angular rate = 0°/sec, dynamic range = ±450°/sec ± 1 g, 300 mbar to 1100 mbar, unless otherwise noted. Table 1. Parameter GYROSCOPES Dynamic Range Sensitivity Repeatability 1 Sensitivity Temperature Coefficient Misalignment Nonlinearity Bias Repeatability1, 2 In-Run Bias Stability Angular Random Walk Bias Temperature Coefficient Linear Acceleration Effect on Bias Output Noise Rate Noise Density 3 dB Bandwidth Sensor Resonant Frequency ACCELEROMETERS Dynamic Range Sensitivity Repeatability1, 3 Sensitivity Temperature Coefficient Misalignment Nonlinearity Bias Repeatability1, 2 In-Run Bias Stability Velocity Random Walk Bias Temperature Coefficient Output Noise Noise Density 3 dB Bandwidth Sensor Resonant Frequency TEMPERATURE SENSOR Scale Factor LOGIC INPUTS 4 Input High Voltage, VIH Input Low Voltage, VIL CS Wake-Up Pulse Width Logic 1 Input Current, IIH Logic 0 Input Current, IIL Test Conditions/Comments Min ±450 x_GYRO_OUT and x_GYRO_LOW (32-bit) −40°C ≤ TA ≤ +85°C −40°C ≤ TA ≤ +85°C, 1 σ Axis-to-axis Axis-to-frame (package) Best fit straight line, FS = 450°/sec −40°C ≤ TA ≤ +85°C, 1 σ 1σ 1σ −40°C ≤ TA ≤ +85°C, 1 σ Any axis, 1 σ (CONFIG[7] = 1) No filtering f = 25 Hz, no filtering Max Unit ±480 °/sec °/sec/LSB % ppm/°C Degrees Degrees % of FS °/sec °/hr °/√hr °/sec/°C °/sec/g °/sec rms °/sec/√Hz rms Hz kHz 3.052 × 10−7 ±1 ±35 ±0.05 ±1.0 0.01 ±0.2 6.25 0.3 ±0.0025 0.009 0.16 0.0066 330 18 Each axis ±5 x_ACCL_OUT and x_ACCL_LOW (32-bit) −40°C ≤ TA ≤ +85°C −40°C ≤ TA ≤ +85C, 1 σ Axis-to-axis Axis-to-frame (package) Best-fit straight line, ±5 g −40°C ≤ TA ≤ +85°C, 1 σ 1σ 1σ −40°C ≤ TA ≤ +85°C No filtering f = 25 Hz, no filtering ±10 ±0.035 ±1.0 0.1 ±3 32 0.023 ±0.03 1.25 0.055 330 5.5 g g/LSB % ppm/°C Degrees Degrees % of FS mg µg m/sec/√hr mg/°C mg rms mg/√Hz rms Hz kHz 0.00565 °C/LSB 3.815 × 10−9 ±0.5 Output = 0x0000 at 25°C (±5°C) 2.0 0.8 20 VIH = 3.3 V VIL = 0 V 10 10 All Pins Except RST and CS RST and CS Pins 5 Input Capacitance, CIN DIGITAL OUTPUTS Output High Voltage, VOH Output Low Voltage, VOL Typ 0.33 10 ISOURCE = 0.5 mA ISINK = 2.0 mA 2.4 0.4 Rev. H | Page 4 of 32 V V µs µA µA mA pF V V Data Sheet Parameter FLASH MEMORY Data Retention 7 FUNCTIONAL TIMES 8 Power-On, Start-Up Time Reset Recovery Time 9 Sleep Mode Recovery Time Flash Memory Update Time Flash Memory Test Time Automatic Self Test Time CONVERSION RATE Initial Clock Accuracy Temperature Coefficient Sync Input Clock 10 POWER SUPPLY, VDD Power Supply Current 11 POWER SUPPLY, VDDRTC Real-Time Clock Supply Current ADIS16485 Test Conditions/Comments Endurance 6 TJ = 85°C Time until data is available Min 100,000 20 Max 400 ± 160 400 ± 160 500 900 66 12 2.46 0.02 40 Using internal clock, 100 SPS Operating voltage range Normal mode, VDD = 3.3 V, µ ± σ Sleep mode, VDD = 3.3 V Power-down mode, VDD = 3.3 V Operating voltage range Normal mode, VDDRTC = 3.3 V Typ 0.7 3.0 2.4 3.6 197 12.2 37 3.0 3.6 13 Unit Cycles Years ms ms µs ms ms ms kSPS % ppm/°C kHz V mA mA µA V µA The repeatability specifications represent analytical projections that are based off of the following drift contributions and conditions: temperature hysteresis (−40°C to +85°C), electronics drift (high temperature operating life test: +110°C, 500 hours), drift from temperature cycling (JESD22, Method A104-C, Method N, 500 cycles, −40°C to +85°C), rate random walk (10 year projection), and broadband noise 2 Bias repeatability describes a long-term behavior over a variety of conditions. Short-term repeatability is related to the in-run bias stability and noise density specifications. 3 X-ray exposure may degrade this performance metric. 4 The digital I/O signals use a 3.3 V system. 5 RST and CS pins are connected to the VDD pin through 10 kΩ pull-up resistors. 6 Endurance is qualified as per JEDEC Standard 22, Method A117, and measured at −40°C, +25°C, +85°C, and +125°C. 7 The data retention specification assumes a junction temperature (TJ) of 85°C as per JEDEC Standard 22, Method A117. Data retention lifetime decreases with TJ. 8 These times do not include thermal settling and internal filter response times, which can affect overall accuracy. 9 The RST line must be in a low state for at least 10 μs to assure a proper reset initiation and recovery. 10 The device functions at clock rates below 0.7 kHz but at reduced performance levels. 11 Supply current transients can reach 600 mA during start-up and reset recovery. 1 Rev. H | Page 5 of 32 ADIS16485 Data Sheet TIMING SPECIFICATIONS TA = 25°C, VDD = 3.3 V, unless otherwise noted. Table 2. Parameter fSCLK tSTALL 2 tCLS tCHS tCS Description Serial clock Stall period between data communication cycles Serial clock low period Serial clock high period Chip select to clock edge tDAV tDSU tDHD tDR, tDF tDSOE tHD tSFS tDSHI t1 t2 t3 DOUT valid after SCLK edge DIN setup time before SCLK rising edge DIN hold time after SCLK rising edge DOUT rise/fall times, ≤100 pF loading CS assertion to data out active SCLK edge to data out invalid Last SCLK edge to CS deassertion CS deassertion to data out high impedance Input sync pulse width Input sync to data invalid Input sync period 1 2 Min 1 0.01 2 31 31 32 Normal Mode Typ Max1 15 Unit MHz µs ns ns ns 10 ns ns ns ns ns ns ns ns µs µs µs 2 2 3 0 0 32 0 5 8 11 9 510 417 Guaranteed by design and characterization, but not tested in production. See Table 3 for exceptions to the stall time rating. Table 3. Register Specific Stall Times Register FNCTIO_CTRL FLTR_BNK0 FLTR_BNK1 NULL_CFG GLOB_CMD[1] GLOB_CMD[2] GLOB_CMD[3] GLOB_CMD[6] GLOB_CMD[7] Function Configure DIOx functions Enable/select FIR filter banks Enable/select FIR filter banks Configure autonull bias function Self test Memory test Flash memory update Flash memory test Software reset Rev. H | Page 6 of 32 Minimum Stall Time (μs) 60 320 320 10 12,000 50,000 375,000 75,000 12,000 Data Sheet ADIS16485 Timing Diagrams CS tCLS tCHS tCS 1 2 3 4 5 tSFS 6 15 16 SCLK DOUT tDAV MSB DB14 tHD DB13 tDSU DIN R/W A6 DB12 tDR DB11 DB10 DB2 tDSHI DB1 tDHD A5 LSB tDF A4 A3 A2 D2 D1 10666-002 tDSOE LSB Figure 2. SPI Timing and Sequence tSTALL 10666-003 CS SCLK Figure 3. Stall Time and Data Rate t2 t3 t1 SYNC CLOCK (CLKIN) OUTPUT REGISTERS DATA VALID DATA VALID Figure 4. Input Clock Timing Diagram Rev. H | Page 7 of 32 10666-004 DATA READY ADIS16485 Data Sheet ABSOLUTE MAXIMUM RATINGS Table 4. Parameter Acceleration Any Axis, Unpowered Any Axis, Powered VDD to GND Digital Input Voltage to GND Digital Output Voltage to GND Operating Temperature Range Storage Temperature Range 1 Rating 2000 g 2000 g −0.3 V to +3.6 V −0.3 V to VDD + 0.2 V −0.3 V to VDD + 0.2 V −40°C to +105°C −65°C to +150°C1 Extended exposure to temperatures that are lower than −40°C or higher than +105°C can adversely affect the accuracy of the factory calibration. Stresses at or above those listed under Absolute Maximum Ratings may cause permanent damage to the product. This is a stress rating only; functional operation of the product at these or any other conditions above those indicated in the operational section of this specification is not implied. Operation beyond the maximum operating conditions for extended periods may affect product reliability. Table 5. Package Characteristics Package Type 24-Lead Module (ML-24-6) ESD CAUTION Rev. H | Page 8 of 32 θJA 22.8°C/W θJC 10.1°C/W Device Weight 48 g Data Sheet ADIS16485 PIN CONFIGURATION AND FUNCTION DESCRIPTIONS ADIS16485 DNC DNC DNC GND VDD VDD RST CS DOUT DIO4 20 18 16 14 12 10 8 6 4 2 23 21 19 17 15 13 11 9 7 5 3 1 DNC DNC GND GND VDD DIO2 DIO1 DIN SCLK NOTES 1. THIS REPRESENTATION DISPLAYS THE TOP VIEW PINOUT FOR THE MATING SOCKET CONNECTOR. 2. THE ACTUAL CONNECTOR PINS ARE NOT VISIBLE FROM THE TOP VIEW. 3. MATING CONNECTOR: SAMTEC CLM-112-02 OR EQUIVALENT. 4. DNC = DO NOT CONNECT. 10666-005 DIO3 DNC 22 DNC 24 VDDRTC DNC TOP VIEW (Not to Scale) Figure 5. Mating Connector Pin Assignments PIN 23 PIN 1 PIN 2 10666-106 PIN 1 Figure 6. Axial Orientation (Top Side Facing Up) Table 6. Pin Function Descriptions Pin No. 1 2 3 4 5 6 7 8 9 10, 11, 12 13, 14, 15 16 to 22, 24 23 Mnemonic DIO3 DIO4 SCLK DOUT DIN CS DIO1 RST DIO2 VDD GND DNC VDDRTC Type Input/output Input/output Input Output Input Input Input/output Input Input/output Supply Supply Not applicable Supply Description Configurable Digital Input/Output. Configurable Digital Input/Output. SPI Serial Clock. SPI Data Output. Clocks output on SCLK falling edge. SPI Data Input. Clocks input on SCLK rising edge. SPI Chip Select. Configurable Digital Input/Output. Reset. Configurable Digital Input/Output. Power Supply. Power Ground. Do Not Connect to These Pins. Real-Time Clock Power Supply. Rev. H | Page 9 of 32 ADIS16485 Data Sheet TYPICAL PERFORMANCE CHARACTERISTICS 1000 0.8 AVERAGE GYRO SCALE ERROR (% FS) 100 +1σ 10 1 10 100 1000 10000 0 –0.2 –0.4 INTEGRATION PERIOD (Seconds) –0.8 –40 –30 –20 –10 10666-007 0.1 0.2 –0.6 –1σ 1 0.01 INITIAL ERROR = ±0.5% 0.4 TEMPCO = 35ppm/°C 0 10 20 30 40 50 60 70 10666-009 ROOT ALLAN VARIANCE (°/Hour) 0.6 80 TEMPERATURE (°C) Figure 9. Gyroscope Scale (Sensitivity) Error and Hysteresis vs. Temperature Figure 7. Gyroscope Allan Variance, 25°C 0.6 1 INITIAL ERROR = ±0.2°/sec 0.5 TEMPCO = 0.0025°/sec/°C AVERAGE GYRO BIAS ERROR (°/sec) ROOT ALLAN VARIANCE (mg) 0.4 +δ 0.1 0.3 0.2 0.1 0 –0.1 –0.2 –0.3 –0.4 –δ 1 1000 10 100 INTEGRATION PERIOD (Seconds) 10000 0 10 20 30 40 50 60 70 80 TEMPERATURE (°C) Figure 10. Gyroscope Bias Error and Hysteresis vs. Temperature Figure 8. Accelerometer Allan Variance, 25°C Rev. H | Page 10 of 32 10666-010 0.1 10666-008 0.01 0.01 –0.5 –0.6 –40 –30 –20 –10 Data Sheet ADIS16485 BASIC OPERATION I/O LINES ARE COMPATIBLE WITH 3.3V LOGIC LEVELS REGISTER STRUCTURE The register structure and SPI port provide a bridge between the sensor processing system and an external, master processor. It contains both output data and control registers. The output data registers include the latest sensor data, a real-time clock, error flags, alarm flags, and identification data. The control registers include sample rate, filtering, input/output, alarms, calibration, and diagnostic configuration options. All communication between the ADIS16485 and an external processor involves either reading or writing to one of the user registers. TRIAXIS GYRO +3.3V VDD DSP OUTPUT REGISTERS 10 SYSTEM PROCESSOR SPI MASTER 11 12 23 TEMP SENSOR ADIS16485 SS 6 CS SCLK 3 SCLK MOSI 5 DIN MISO 4 DOUT IRQ 9 DIO2 15 10666-011 14 Figure 11. Electrical Connection Diagram Table 7. Generic Master Processor Pin Names and Functions Function Slave select Interrupt request Master output, slave input Master input, slave output Serial clock CONTROL REGISTERS The register structure uses a paged addressing scheme that is composed of 13 pages, with each one containing 64 register locations. Each register is 16 bits wide, with each byte having its own unique address within the memory map of that page. The SPI port has access to one page at a time, using the bit sequence in Figure 17. Select the page to activate for SPI access by writing its code to the PAGE_ID register. Read the PAGE_ID register to determine which page is currently active. Table 9 displays the PAGE_ID contents for each page, together with their basic functions. The PAGE_ID register is located at Address 0x00 on every page. Table 9. User Register Page Assignments Embedded processors typically use control registers to configure their serial ports for communicating with SPI slave devices such as the ADIS16485. Table 8 provides a list of settings, which describe the SPI protocol of the ADIS16485. The initialization routine of the master processor typically establishes these settings using firmware commands to write them into its serial control registers. Table 8. Generic Master Processor SPI Settings Processor Setting Master SCLK ≤ 15 MHz SPI Mode 3 MSB-First Mode 16-Bit Mode CONTROLLER Figure 12. Basic Operation 13 Mnemonic SS IRQ MOSI MISO SCLK SPI TRIAXIS ACCEL 10666-012 The ADIS16485 is an autonomous sensor system that starts up on its own when it has a valid power supply. After running through its initialization process, it begins sampling, processing, and loading calibrated sensor data into the output registers, which are accessible using the SPI port. The SPI port typically connects to a compatible port on an embedded processor, using the connection diagram in Figure 11. The four SPI signals facilitate synchronous, serial data communication. Connect RST (Pin 8, see Table 6) to VDD or leave RST open for normal operation. The factory default configuration provides users with a data-ready signal on the DIO2 pin, which pulses high when new data is available in the output data registers. Description ADIS16485 operates as slave Maximum serial clock rate CPOL = 1 (polarity), and CPHA = 1 (phase) Bit sequence Shift register/data length Page 0 1 2 3 4 5 6 7 8 9 10 11 12 Rev. H | Page 11 of 32 PAGE_ID 0x00 0x01 0x02 0x03 0x04 0x05 0x06 0x07 0x08 0x09 0x0A 0x0B 0x0C Function Output data, clock, identification Reserved Calibration Control: sample rate, filtering, I/O, alarms Serial number FIR Filter Bank A Coefficient 0 to Coefficient 59 FIR Filter Bank A, Coefficient 60 to Coefficient 119 FIR Filter Bank B, Coefficient 0 to Coefficient 59 FIR Filter Bank B, Coefficient 60 to Coefficient 119 FIR Filter Bank C, Coefficient 0 to Coefficient 59 FIR Filter Bank C, Coefficient 60 to Coefficient 119 FIR Filter Bank D, Coefficient 0 to Coefficient 59 FIR Filter Bank D, Coefficient 60 to Coefficient 119 ADIS16485 Data Sheet SPI COMMUNICATION MANUAL FLASH BACKUP The SPI port supports full duplex communication, as shown in Figure 17, which enables external processors to write to DIN while reading DOUT, when the previous command was a read request. Figure 17 provides a guideline for the bit coding on both DIN and DOUT. NONVOLATILE FLASH MEMORY (NO SPI ACCESS) The SPI provides write access to the control registers, one byte at a time, using the bit assignments shown in Figure 17. Each register has 16 bits, where Bits[7:0] represent the lower address (listed in Table 10) and Bits[15:8] represent the upper address. Write to the lower byte of a register first, followed by a write to its upper byte. The only register that changes with a single write to its lower byte is the PAGE_ID register. For a write command, the first bit in the DIN sequence is set to 1. Address Bits[A6:A0] represent the target address, and Data Command Bits[DC7:DC0] represent the data being written to the location. Figure 13 provides an example of writing 0x03 to Address 0x00 (PAGE_ID [7:0]), using DIN = 0x8003. This write command activates the control page for SPI access. 10666-014 Figure 14. SRAM and Flash Memory Diagram READING SENSOR DATA 10666-013 SCLK DIN Figure 13. SPI Sequence for Activating the Control Page (DIN = 0x8003) 0x1A00 DOUT Dual Memory Structure 0x1800 NEXT ADDRESS Z_GYRO_OUT Z_GYRO_LOW Figure 15. SPI Read Example Writing configuration data to a control register updates its SRAM contents, which are volatile. After optimizing each relevant control register setting in a system, use the manual flash update command, which is located in GLOB_CMD[3] on Page 3 of the register map. Activate the manual flash update command by turning to Page 3 (DIN = 0x8003) and setting GLOB_CMD[3] = 1 (DIN = 0x8208, then DIN = 0x8300). Make sure that the power supply is within specification for the entire 375 ms processing time for a flash memory update. Table 10 provides a memory map for all of the user registers, which includes a column of flash backup information. A yes in this column indicates that a register has a mirror location in flash and, when backed up properly, automatically restores itself during startup or after a reset. Figure 14 provides a diagram of the dual memory structure used to manage operation and store critical user settings. Figure 16 provides an example of the four SPI signals when reading PROD_ID in a repeating pattern. This is a good pattern to use for troubleshooting the SPI interface setup and communications because the contents of PROD_ID are predefined and stable. CS SCLK DIN DOUT DOUT = 0100 0000 0110 0101 = 0x4065 = 16,485 (PROD_ID) Figure 16. SPI Read Example, Second 16-Bit Sequence CS D15 A6 A5 A4 A3 A2 A1 A0 DC7 DC6 DC5 DC4 DC3 DC2 DC1 DC0 D14 D13 D12 D11 D10 D9 D8 D7 D6 D5 D4 D3 D2 D1 D0 R/W D15 A6 A5 D14 D13 NOTES 1. DOUT BITS ARE PRODUCED ONLY WHEN THE PREVIOUS 16-BIT DIN SEQUENCE STARTS WITH R/W = 0. 2. WHEN CS IS HIGH, DOUT IS IN A THREE-STATE, HIGH IMPEDANCE MODE, WHICH ALLOWS MULTIFUNCTIONAL USE OF THE LINE FOR OTHER DEVICES. Figure 17. SPI Communication Bit Sequence Rev. H | Page 12 of 32 10666-017 DOUT R/W 10666-016 DIN = 0111 1110 0000 0000 = 0x7E00 SCLK DIN 10666-015 The ADIS16485 automatically starts up and activates Page 0 for data register access. Write 0x00 to the PAGE_ID register (DIN = 0x8000) to activate Page 0 for data access after accessing any other page. A single register read requires two 16-bit SPI cycles. The first cycle requests the contents of a register using the bit assignments in Figure 17, and then the register contents follow DOUT during the second sequence. The first bit in a DIN command is zero, followed by either the upper or the lower address for the register. The last eight bits are don’t care, but the SPI requires the full set of 16 SCLKs to receive the request. Figure 15 includes two register reads in succession, which starts with DIN = 0x1A00 to request the contents of the Z_GYRO_OUT register and follows with 0x1800 to request the contents of the Z_GYRO_LOW register. CS DIN = 1000 0000 0000 0011 = 0x8003, WRITES 0x03 TO ADDRESS 0x00 SPI ACCESS START-UP RESET DEVICE CONFIGURATION DIN VOLATILE SRAM Data Sheet ADIS16485 USER REGISTERS Table 10. User Register Memory Map (N/A Means Not Applicable) Name PAGE_ID Reserved SYS_E_FLAG DIAG_STS ALM_STS TEMP_OUT X_GYRO_LOW X_GYRO_OUT Y_GYRO_LOW Y_GYRO_OUT Z_GYRO_LOW Z_GYRO_OUT X_ACCL_LOW X_ACCL_OUT Y_ACCL_LOW Y_ACCL_OUT Z_ACCL_LOW Z_ACCL_OUT Reserved X_DELTANG_LOW X_DELTANG_OUT Y_DELTANG_LOW Y_DELTANG_OUT Z_DELTANG_LOW Z_DELTANG_OUT X_DELTVEL_LOW X_DELTVEL_OUT Y_DELTVEL_LOW Y_DELTVEL_OUT Z_DELTVEL_LOW Z_DELTVEL_OUT Reserved TIME_MS_OUT TIME_DH_OUT TIME_YM_OUT PROD_ID Reserved PAGE_ID Reserved X_GYRO_SCALE Y_GYRO_SCALE Z_GYRO_SCALE X_ACCL_SCALE Y_ACCL_SCALE Z_ACCL_SCALE R/W R/W N/A R R R R R R R R R R R R R R R R N/A R R R R R R R R R R R R N/A R R R R N/A R/W N/A R/W R/W R/W R/W R/W R/W Flash No N/A No No No No No No No No No No No No No No No No N/A No No No No No No No No No No No No N/A Yes Yes Yes Yes N/A No N/A Yes Yes Yes Yes Yes Yes PAGE_ID 0x00 0x00 0x00 0x00 0x00 0x00 0x00 0x00 0x00 0x00 0x00 0x00 0x00 0x00 0x00 0x00 0x00 0x00 0x00 0x00 0x00 0x00 0x00 0x00 0x00 0x00 0x00 0x00 0x00 0x00 0x00 0x00 0x00 0x00 0x00 0x00 0x01 0x02 0x02 0x02 0x02 0x02 0x02 0x02 0x02 Address 0x00 0x02 to 0x06 0x08 0x0A 0x0C 0x0E 0x10 0x12 0x14 0x16 0x18 0x1A 0x1C 0x1E 0x20 0x22 0x24 0x26 0x28 to 0x3E 0x40 0x42 0x44 0x46 0x48 0x4A 0x4C 0x4E 0x50 0x52 0x54 0x56 0x58 to 0x76 0x78 0x7A 0x7C 0x7E 0x00 to 0x7E 0x00 0x02 0x04 0x06 0x08 0x0A 0x0C 0x0E Default 0x00 N/A 0x0000 0x0000 0x0000 N/A N/A N/A N/A N/A N/A N/A N/A N/A N/A N/A N/A N/A N/A N/A N/A N/A N/A N/A N/A N/A N/A N/A N/A N/A N/A N/A N/A N/A N/A 0x4065 N/A 0x00 N/A 0x0000 0x0000 0x0000 0x0000 0x0000 0x0000 Register Description Page identifier Reserved Output, system error flags Output, self test error flags Output, alarm error flags Output, temperature Output, x-axis gyroscope, low word Output, x-axis gyroscope, high word Output, y-axis gyroscope, low word Output, y-axis gyroscope, high word Output, z-axis gyroscope, low word Output, z-axis gyroscope, high word Output, x-axis accelerometer, low word Output, x-axis accelerometer, high word Output, y-axis accelerometer, low word Output, y-axis accelerometer, high word Output, z-axis accelerometer, low word Output, z-axis accelerometer, high word Reserved Output, x-axis delta angle, low word Output, x-axis delta angle, high word Output, y-axis delta angle, low word Output, y-axis delta angle, high word Output, z-axis delta angle, low word Output, z-axis delta angle, high word Output, x-axis delta velocity, low word Output, x-axis delta velocity, high word Output, y-axis delta velocity, low word Output, y-axis delta velocity, high word Output, z-axis delta velocity, low word Output, z-axis delta velocity, high word Reserved Factory configuration time: minutes/seconds Factory configuration date/time: day/hour Factory configuration date: year/month Output, product identification (16,485) Reserved Page identifier Reserved Calibration, scale, x-axis gyroscope Calibration, scale, y-axis gyroscope Calibration, scale, z-axis gyroscope Calibration, scale, x-axis accelerometer Calibration, scale, y-axis accelerometer Calibration, scale, z-axis accelerometer Rev. H | Page 13 of 32 Format N/A N/A Table 41 Table 42 Table 43 Table 39 Table 15 Table 11 Table 16 Table 12 Table 17 Table 13 Table 22 Table 18 Table 23 Table 19 Table 24 Table 20 N/A Table 29 Table 25 Table 30 Table 26 Table 31 Table 27 Table 36 Table 32 Table 37 Table 33 Table 38 Table 34 N/A Table 96 Table 97 Table 98 Table 47 N/A N/A N/A Table 64 Table 65 Table 66 Table 74 Table 75 Table 76 ADIS16485 Name 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 ZA_BIAS_HIGH Reserved USER_SCR_1 USER_SCR_2 USER_SCR_3 USER_SCR_4 FLSHCNT_LOW FLSHCNT_HIGH PAGE_ID GLOB_CMD Reserved FNCTIO_CTRL GPIO_CTRL CONFIG DEC_RATE NULL_CNFG SLP_CNT Reserved FILTR_BNK_0 FILTR_BNK_1 Reserved ALM_CNFG_0 ALM_CNFG_1 Reserved XG_ALM_MAGN YG_ALM_MAGN ZG_ALM_MAGN XA_ALM_MAGN YA_ALM_MAGN ZA_ALM_MAGN Reserved FIRM_REV FIRM_DM FIRM_Y Reserved Reserved SERIAL_NUM Reserved Data Sheet R/W R/W R/W R/W R/W R/W R/W R/W R/W R/W R/W R/W R/W N/A R/W R/W R/W R/W R R R/W W N/A R/W R/W R/W R/W R/W R/W N/A R/W R/W N/A R/W R/W N/A R/W R/W R/W R/W R/W R/W N/A R R R N/A N/A R N/A Flash Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes N/A Yes Yes Yes Yes Yes Yes No No N/A Yes Yes Yes Yes Yes No N/A Yes Yes N/A Yes Yes N/A Yes Yes Yes Yes Yes Yes N/A Yes Yes Yes N/A N/A Yes N/A PAGE_ID 0x02 0x02 0x02 0x02 0x02 0x02 0x02 0x02 0x02 0x02 0x02 0x02 0x02 0x02 0x02 0x02 0x02 0x02 0x02 0x03 0x03 0x03 0x03 0x03 0x03 0x03 0x03 0x03 0x03 0x03 0x03 0x03 0x03 0x03 0x03 0x03 0x03 0x03 0x03 0x03 0x03 0x03 0x03 0x03 0x03 0x03 0x04 0x04 0x04 Address 0x10 0x12 0x14 0x16 0x18 0x1A 0x1C 0x1E 0x20 0x22 0x24 0x26 0x28 to 0x72 0x74 0x76 0x78 0x7A 0x7C 0x7E 0x00 0x02 0x04 0x06 0x08 0x0A 0x0C 0x0E 0x10 0x12 to 0x14 0x16 0x18 0x1A to 0x1E 0x20 0x22 0x24 to 0x26 0x28 0x2A 0x2C 0x2E 0x30 0x32 0x34 to 0x76 0x78 0x7A 0x7C 0x7E 0x00 to 0x18 0x20 0x22 to 0x7F Default 0x0000 0x0000 0x0000 0x0000 0x0000 0x0000 0x0000 0x0000 0x0000 0x0000 0x0000 0x0000 N/A 0x0000 0x0000 0x0000 0x0000 N/A N/A 0x0000 N/A N/A 0x000D 0x00X0 1 0x00C0 0x0000 0x070A N/A N/A 0x0000 0x0000 N/A 0x0000 0x0000 N/A 0x0000 0x0000 0x0000 0x0000 0x0000 0x0000 N/A N/A N/A N/A N/A N/A N/A N/A Register Description Calibration, offset, gyroscope, x-axis, low word Calibration, offset, gyroscope, x-axis, high word Calibration, offset, gyroscope, y-axis, low word Calibration, offset, gyroscope, y-axis, high word Calibration, offset, gyroscope, z-axis, low word Calibration, offset, gyroscope, z-axis, high word Calibration, offset, accelerometer, x-axis, low word Calibration, offset, accelerometer, x-axis, high word Calibration, offset, accelerometer, y-axis, low word Calibration, offset, accelerometer, y-axis, high word Calibration, offset, accelerometer, z-axis, low word Calibration, offset, accelerometer, z-axis, high word Reserved User Scratch Register 1 User Scratch Register 2 User Scratch Register 3 User Scratch Register 4 Diagnostic, flash memory count, low word Diagnostic, flash memory count, high word Page identifier Control, global commands Reserved Control, I/O pins, functional definitions Control, I/O pins, general purpose Control, clock, and miscellaneous correction Control, output sample rate decimation Control, automatic bias correction configuration Control, power-down/sleep mode Reserved Filter selection Filter selection Reserved Alarm configuration Alarm configuration Reserved Alarm, x-axis gyroscope threshold setting Alarm, y-axis gyroscope threshold setting Alarm, z-axis gyroscope threshold setting Alarm, x-axis accelerometer threshold Alarm, y-axis accelerometer threshold Alarm, z-axis accelerometer threshold Reserved Firmware revision Firmware programming date: day/month Firmware programming date: year Reserved Reserved Serial number Reserved Rev. H | Page 14 of 32 Format Table 60 Table 57 Table 61 Table 58 Table 62 Table 59 Table 71 Table 68 Table 72 Table 69 Table 73 Table 70 N/A Table 92 Table 93 Table 94 Table 95 Table 87 Table 88 N/A Table 86 N/A Table 89 Table 90 Table 67 Table 49 Table 63 Table 91 N/A Table 50 Table 51 N/A Table 83 Table 84 N/A Table 77 Table 78 Table 79 Table 80 Table 81 Table 82 N/A Table 44 Table 45 Table 46 N/A N/A Table 48 N/A Data Sheet Name PAGE_ID FIR_COEF_Axxx PAGE_ID FIR_COEF_Axxx PAGE_ID FIR_COEF_Bxxx PAGE_ID FIR_COEF_Bxxx PAGE_ID FIR_COEF_Cxxx PAGE_ID FIR_COEF_Cxxx PAGE_ID FIR_COEF_Dxxx PAGE_ID FIR_COEF_Dxxx 1 ADIS16485 R/W R/W R/W R/W R/W R/W R/W R/W R/W R/W R/W R/W R/W R/W R/W R/W R/W Flash No Yes No Yes No Yes No Yes No Yes No Yes No Yes No Yes PAGE_ID 0x05 0x05 0x06 0x06 0x07 0x07 0x08 0x08 0x09 0x09 0x0A 0x0A 0x0B 0x0B 0x0C 0x0C Address 0x00 0x02 to 0x7E 0x00 0x02 to 0x7E 0x00 0x02 to 0x7E 0x00 0x02 to 0x7E 0x00 0x02 to 0x7E 0x00 0x02 to 0x7E 0x00 0x02 to 0x7E 0x00 0x02 to 0x7E Default 0x0000 N/A 0x0000 N/A 0x0000 N/A 0x0000 N/A 0x0000 N/A 0x0000 N/A 0x0000 N/A 0x0000 N/A Register Description Page identifier FIR Filter Bank A, Coefficients 0 through 59 Page identifier FIR Filter Bank A, Coefficients 60 through 119 Page identifier FIR Filter Bank B, Coefficients 0 through 59 Page identifier FIR Filter Bank B, Coefficients 60 through 119 Page identifier FIR Filter Bank C, Coefficients 0 through 59 Page identifier FIR Filter Bank C, Coefficients 60 through 119 Page identifier FIR Filter Bank D, Coefficients 0 through 59 Page identifier FIR Filter Bank D, Coefficients 60 through 119 The GPIO_CTRL[7:4] bits reflect the logic levels on the DIOx lines and do not have a default setting. Rev. H | Page 15 of 32 Format N/A Table 52 N/A Table 52 N/A Table 53 N/A Table 53 N/A Table 54 N/A Table 54 N/A Table 55 N/A Table 55 ADIS16485 Data Sheet OUTPUT DATA REGISTERS After the ADIS16485 completes its start-up process, the PAGE_ID register contains 0x0000, which sets Page 0 as the active page for SPI access. Page 0 contains the output data, real-time clock, status, and product identification registers. Table 12. Y_GYRO_OUT (Page 0, Base Address = 0x16) Bits [15:0] Description Y-axis gyroscope data; twos complement, ±450°/sec range, 0°/sec = 0x0000, 1 LSB = 0.02°/sec INERTIAL SENSOR DATA FORMAT Table 13. Z_GYRO_OUT (Page 0, Base Address = 0x1A) The gyroscope, accelerometer, delta angle, and delta velocity output data registers use a 32-bit, twos complement format. Each output uses two registers to support this resolution. Figure 18 provides an example of how each register contributes to each inertial measurement. In this case, X_GYRO_OUT is the most significant word (upper 16 bits), and X_GYRO_LOW is the least significant word (lower 16 bits). In many cases, using the most significant word registers alone provide sufficient resolution for preserving key performance metrics. Rotation Rate +450°/sec +0.04/sec +0.02°/sec 0°/sec −0.02°/sec −0.04°/sec −450°/sec X_GYRO_LOW 0 15 0 X-AXIS GYROSCOPE DATA Description Z-axis gyroscope data; twos complement, ±450°/sec range, 0°/sec = 0x0000, 1 LSB = 0.02°/sec Table 14. X_GYRO_OUT Data Format Examples 10666-021 X_GYRO_OUT 15 Bits [15:0] Figure 18. Gyroscope Output Format Example, DEC_RATE > 0 Decimal +22,500 +2 +1 0 −1 −2 −22,500 Hex 0x57E4 0x0002 0x0001 0x0000 0xFFFF 0xFFFE 0xA81C Binary 0101 0111 1110 0100 0000 0000 0000 0010 0000 0000 0000 0001 0000 0000 0000 0000 1111 1111 1111 1111 1111 1111 1111 1110 1010 1000 0001 1100 The registers that use the x_GYRO_LOW naming format provide additional resolution for the gyroscope measurements (see Table 15, Table 16, and Table 17). The MSB has a weight of 0.01°/sec, and each subsequent bit has ½ the weight of the previous one. The arrows in Figure 19 describe the direction of the motion, which produces a positive output response in each output register of the sensor. The accelerometers respond to both dynamic and static forces associated with acceleration, including gravity. When lying perfectly flat, as shown in Figure 19, the z-axis accelerometer output is 1 g, and the x and y accelerometers are 0 g. Table 15. X_GYRO_LOW (Page 0, Base Address = 0x10) Bits [15:0] ROTATION RATE (GYROSCOPE) The registers that use the x_GYRO_OUT format are the primary registers for the gyroscope measurements (see Table 11, Table 12, and Table 13). When processing data from these registers, use a 16-bit, twos complement data format. Table 14 provides x_GYRO_OUT digital coding examples. Description X-axis gyroscope data; additional resolution bits Table 16. Y_GYRO_LOW (Page 0, Base Address = 0x14) Bits [15:0] Description Y-axis gyroscope data; additional resolution bits Table 17. Z_GYRO_LOW (Page 0, Base Address = 0x18) Table 11. X_GYRO_OUT (Page 0, Base Address = 0x12) Bits [15:0] Description X-axis gyroscope data; twos complement, ±450°/sec range, 0°/sec = 0x0000, 1 LSB = 0.02°/sec Description Z-axis gyroscope data; additional resolution bits Z-AXIS aZ gZ X-AXIS Y-AXIS gX aY gY PIN 23 aX 10666-119 Bits [15:0] PIN 1 Figure 19. Inertial Sensor Direction Reference Diagram Rev. H | Page 16 of 32 Data Sheet ADIS16485 ACCELERATION The registers that use the x_ACCL_OUT format are the primary registers for the accelerometer measurements (see Table 18, Table 19, and Table 20). When processing data from these registers, use a 16-bit, twos complement data format. Table 21 provides x_ACCL_OUT digital coding examples. Table 18. X_ACCL_OUT (Page 0, Base Address = 0x1E) Bits [15:0] Description X-axis accelerometer data; twos complement, ±5 g range, 0 g = 0x0000, 1 LSB = 0.25 mg Table 19. Y_ACCL_OUT (Page 0, Base Address = 0x22) Bits [15:0] Description Z-axis accelerometer data; twos complement, ±5 g range, 0 g = 0x0000, 1 LSB = 0.25 mg Table 21. x_ACCL_OUT Data Format Examples Acceleration +5 g +0.5 mg +0.25 mg 0 mg −0.25 mg −0.5 mg −5 g Decimal +20,000 +2 +1 0 −1 −2 −20,000 Hex 0x4E20 0x0002 0x0001 0x0000 0xFFFF 0xFFFE 0xB1E0 Binary 0100 1110 0010 0000 0000 0000 0000 0010 0000 0000 0000 0001 0000 0000 0000 0000 1111 1111 1111 1111 1111 1111 1111 1110 1011 0001 1110 0000 The registers that use the x_ACCL_LOW naming format provide additional resolution for the accelerometer measurements (see Table 22, Table 23, and Table 24). The MSB has a weight of 0.125 mg, and each subsequent bit has ½ the weight of the previous one. Table 22. X_ACCL_LOW (Page 0, Base Address = 0x1C) Bits [15:0] Description X-axis accelerometer data; additional resolution bits Description Y-axis accelerometer data; additional resolution bits Table 24. Z_ACCL_LOW (Page 0, Base Address = 0x24) Bits [15:0]  1 D1   x ,n Dd 1 2 f S d 0 x , n D  d  where: D is the decimation rate = DEC_RATE + 1. fS is the sample rate. d is the incremental variable in the summation formula. ωx is the x-axis rate of rotation (gyroscope). n is the sample time, prior to the decimation filter. The x_DELTANG_LOW registers (see Table 29, Table 30, and Table 31) provide additional resolution bits for the delta angle and combine with the x_DELTANG_OUT registers to provide a 32-bit, twos complement number. The MSB in the x_DELTANG_LOW registers have a weight of ~0.011° (720°/216), and each subsequent bit carries a weight of ½ of the previous one. Table 25. X_DELTANG_OUT (Page 0, Base Address = 0x42) Bits [15:0] Description X-axis delta angle data; twos complement, ±720° range, 0° = 0x0000, 1 LSB = 720°/215 = ~0.022° Table 26. Y_DELTANG_OUT (Page 0, Base Address = 0x46) Bits [15:0] Description Y-axis delta angle data; twos complement, ±720° range, 0° = 0x0000, 1 LSB = 720°/215 = ~0.022° Table 27. Z_DELTANG_OUT (Page 0, Base Address = 0x4A) Bits [15:0] Description Z-axis delta angle data; twos complement, ±720° range, 0° = 0x0000, 1 LSB = 720°/215 = ~0.022° Table 28. x_DELTANG_OUT Data Format Examples Table 23. Y_ACCL_LOW (Page 0, Base Address = 0x20) Bits [15:0]  x ,n D  When using the internal sample clock, fS is equal to 2460 SPS. When using the external clock option, fS is equal to the frequency of the external clock, which is limited to a minimum of 2 kHz, to prevent overflow in the x_DELTANG_xxx registers at high rotation rates. See Table 49 and Figure 20 for more information on the DEC_RATE register (decimation filter). Description Y-axis accelerometer data; twos complement, ±5 g range, 0 g = 0x0000, 1 LSB = 0.25 mg Table 20. Z_ACCL_OUT (Page 0, Base Address = 0x26) Bits [15:0] The delta angle outputs represent an integration of the gyroscope measurements and use the following formula for all three axes (x-axis displayed): Description Z-axis accelerometer data; additional resolution bits DELTA ANGLES The x_DELTANG_OUT registers are the primary output registers for the delta angle calculations. When processing data from these registers, use a 16-bit, twos complement data format (see Table 25, Table 26, and Table 27). Table 28 shows x_DELTANG_OUT digital coding examples. Angle (°) +720 × (215 − 1)/215 +1440/215 +720/215 0 −720/215 −1440/215 −720 Decimal +32,767 +2 +1 0 −1 −2 −32,768 Hex 0x7FFF 0x0002 0x0001 0x0000 0xFFFF 0xFFFE 0x8000 Binary 0111 1111 1111 1111 0000 0000 0000 0010 0000 0000 0000 0001 0000 0000 0000 0000 1111 1111 1111 1111 1111 1111 1111 1110 1000 0000 0000 0000 The x_DELTANG_LOW registers (see Table 29, Table 30, and Table 31) provide additional resolution for the angle measurement and combine with the x_DELTANT_OUT registers to provide a 32-bit, twos complement number. The MSBs in the x_DELTANG_LOW registers have a weight of ~0.011° (720°/216), and each subsequent bit carries a weight of ½ of the previous one. Rev. H | Page 17 of 32 ADIS16485 Data Sheet Table 29. X_DELTANG_LOW (Page 0, Base Address = 0x40) Bits [15:0] Description X-axis delta angle data; additional resolution bits Table 34. Z_DELTVEL_OUT (Page 0, Base Address = 0x56) Bits [15:0] Table 30. Y_DELTANG_LOW (Page 0, Base Address = 0x44) Bits [15:0] Description Y-axis delta angle data; additional resolution bits Table 35. x_DELTVEL_OUT, Data Format Examples Table 31. Z_DELTANG_LOW (Page 0, Base Address = 0x48) Bits [15:0] Description Z-axis delta angle data; additional resolution bits DELTA VELOCITY The registers that use the x_DELTVEL_OUT format are the primary registers for the delta velocity calculations. When processing data from these registers, use a 16-bit, twos complement data format (see Table 32, Table 33, and Table 34). Table 35 provides x_DELTVEL_OUT digital coding examples. The delta velocity outputs represent an integration of the accelerometer measurements and use the following formula for all three axes (x-axis displayed): ∆Vx ,n D = ( 1 D −1 ×∑ a + a x ,n D + d −1 2 f S d = 0 x ,n D + d ) Hex 0x7FFF 0x0002 0x0001 0x0000 0xFFFF 0xFFFE 0x8000 Binary 0111 1111 1111 1111 0000 0000 0000 0010 0000 0000 0000 0001 0000 0000 0000 0000 1111 1111 1111 1111 1111 1111 1111 1110 1000 0000 0000 0000 Description X-axis delta velocity data; additional resolution bits Table 37. Y_DELTVEL_LOW (Page 0, Base Address = 0x50) Table 32. X_DELTVEL_OUT (Page 0, Base Address = 0x4E) Description X-axis delta velocity data; twos complement, ±50 m/sec range, 0 m/sec = 0x0000, 1 LSB = 50 m/sec ÷ (215 – 1) = ~1.526 mm/sec Table 33. Y_DELTVEL_OUT (Page 0, Base Address = 0x52) Description Y-axis delta velocity data; twos complement, ±50 m/sec range, 0 m/sec = 0x0000, 1 LSB = 50 m/sec ÷ (215 – 1) = ~1.526 mm/sec Decimal +32,767 +2 +1 0 −1 −2 −32,768 The x_DELTVEL_LOW registers (see Table 36, Table 37, and Table 38) provide additional resolution bits for the delta-velocity measurement and combine with the x_DELTVEL_OUT registers to provide a 32-bit, twos complement number. The MSBs in the x_DELTVEL_LOW registers have a weight of ~0.7629 mm/sec (50 m/sec ÷ 216), and each subsequent bit carries a weight of ½ of the previous one. Bits [15:0] When using the internal sample clock, fS is equal to 2460 SPS. When using the external clock option, fS is equal to the frequency of the external clock, which is limited to a minimum of 2 kHz, to prevent overflow in the x_DELTVEL_xxx registers at high rotation rates. See Table 49 and Figure 20 for more information on the DEC_RATE register (decimation filter). Bits [15:0] Velocity (m/sec) +50 × (215 − 1)/215 +100/215 +50/215 0 −50/215 −100/215 −50 Table 36. X_DELTVEL_LOW (Page 0, Base Address = 0x4C) where: ax is the x-axis linear acceleration. fS is the sample rate. n is the sample time, prior to the decimation filter. D is the decimation rate = DEC_RATE + 1. d is the incremental variable in the summation formula. Bits [15:0] Description Z-axis delta velocity data; twos complement, ±50 m/sec range, 0 m/sec = 0x0000, 1 LSB = 50 m/sec ÷ (215 – 1) = ~1.526 mm/sec Bits [15:0] Description Y-axis delta velocity data; additional resolution bits Table 38. Z_DELTVEL_LOW (Page 0, Base Address = 0x54) Bits [15:0] Description Z-axis delta velocity data; additional resolution bits INTERNAL TEMPERATURE The TEMP_OUT register provides an internal temperature measurement that can be useful for observing relative temperature changes inside of the ADIS16485 (see Table 39). Table 40 provides TEMP_OUT digital coding examples. Note that this temperature reflects a higher temperature than ambient, due to self heating. Table 39. TEMP_OUT (Page 0, Base Address = 0x0E) Bits [15:0] Description Temperature data; twos complement, 0.00565°C per LSB, 25°C = 0x0000 Table 40. TEMP_OUT Data Format Examples Temperature (°C) +85 +25 + 0.0113 +25 + 0.00565 +25 +25 − 0.00565 Rev. H | Page 18 of 32 Decimal +10,619 +2 +1 0 −1 Hex 0x297B 0x0002 0x0001 0x0000 0xFFFF Binary 0010 1001 0111 1011 0000 0000 0000 0010 0000 0000 0000 0001 0000 0000 0000 0000 1111 1111 1111 1111 Data Sheet Temperature (°C) +25 − 0.0113 −40 ADIS16485 Decimal −2 −11,504 Hex 0xFFFE 0xD310 Binary 1111 1111 1111 1110 1101 0011 0001 0000 Bits 1 0 Description (Default = 0x0000) Y-axis gyroscope alarm flag (1 = alarm is active) X-axis gyroscope alarm flag (1 = alarm is active) STATUS/ALARM INDICATORS FIRMWARE REVISION The SYS_E_FLAG register in Table 41 provides the system error flags for a variety of conditions (see Table 41). Reading the SYS_E_FLAG register clears all of its error flags and returns each bit to a zero value, with the exception of Bit[7]. If SYS_E_FLAG[7] is high, use the software reset (GLOB_CMD[7], see Table 86) to clear this condition and restore normal operation. If any bit in the SYS_E_FLAG register is associated with an error condition that remains after reading this register, this bit automatically returns to an alarm value as 1. The FIRM_REV register (see Table 44) provides the firmware revision for the internal processor. Each nibble represents a digit in this revision code. For example, if FIRM_REV = 0x0102, the firmware revision is 1.02. Table 41. SYS_E_FLAG (Page 0, Base Address = 0x08) Bits 15 [14:8] 7 6 5 4 3 [2:1] 0 Description (Default = 0x0000) Watch dog timer flag (1 = timed out) Not used Processing overrun (1 = error) Flash memory update, result of GLOB_CMD[3] = 1 (1 = failed update, 0 = update successful) Inertial self test failure (1 = DIAG_STS ≠ 0x0000) Sensor overrange (1 = at least one sensor overranged) SPI communication error (1 = error condition, when the number of SCLK pulses is not equal to a multiple of 16) Not used Alarm status flag (1 = ALM_STS ≠ 0x0000) The DIAG_STS register in Table 42 provides the flags for the internal self test function, which is from GLOB_CMD[1] (see Table 86). Note that reading DIAG_STS also resets it to 0x0000. Table 42. DIAG_STS (Page 0, Base Address = 0x0A) Bits [15:6] 5 4 3 2 1 0 Description (Default = 0x0000) Not used Self test failure, z-axis accelerometer (1 = failure) Self test failure, y-axis accelerometer (1 = failure) Self test failure, x-axis accelerometer (1 = failure) Self test failure, z-axis gyroscope (1 = failure) Self test failure, y-axis gyroscope (1 = failure) Self test failure, x-axis gyroscope (1 = failure) Table 44. FIRM_REV (Page 3, Base Address = 0x78) Bits [15:12] [11:8] [7:4] [3:0] Description Binary, revision, 10s digit Binary, revision, 1s digit Binary, revision, tenths digit Binary, revision, hundredths digit The FIRM_DM register (see Table 45) contains the month and day of the factory configuration date. FIRM_DM[15:12] and FIRM_DM[11:8] contain digits that represent the month of factory configuration. For example, November is the 11th month in a year and represented by FIRM_DM[15:8] = 0x11. FIRM_DM[7:4] and FIRM_DM[3:0] contain digits that represent the day of factory configuration. For example, the 27th day of the month is represented by FIRM_DM[7:0] = 0x27. Table 45. FIRM_DM (Page 3, Base Address = 0x7A) Bits [15:12] [11:8] [7:4] [3:0] Description Binary, month 10s digit, range: 0 to 1 Binary, month 1s digit, range: 0 to 9 Binary, day 10s digit, range: 0 to 3 Binary, day 1s digit, range: 0 to 9 The FIRM_Y register (see Table 46) contains the year of the factory configuration date. For example, the year of 2013 is represented by FIRM_Y = 0x2013. Table 46. FIRM_Y (Page 3, Base Address = 0x7C) Bits [15:12] [11:8] [7:4] [3:0] Description Binary, year 1000s digit, range: 0 to 9 Binary, year 100s digit, range: 0 to 9 Binary, year 10s digit, range: 0 to 9 Binary, year 1s digit, range: 0 to 9 PRODUCT IDENTIFICATION The ALM_STS register in Table 43 provides the alarm bits for the programmable alarm levels of each sensor. Note that reading ALM_STS also resets its value to 0x0000. Table 43. ALM_STS (Page 0, Base Address = 0x0C) Bits [15:6] 5 4 3 2 Description (Default = 0x0000) Not used Z-axis accelerometer alarm flag (1 = alarm is active) Y-axis accelerometer alarm flag (1 = alarm is active) X-axis accelerometer alarm flag (1 = alarm is active) Z-axis gyroscope alarm flag (1 = alarm is active) The PROD_ID register (see Table 47) contains the binary equivalent of the device number (16,485 = 0x4065), and the SERIAL_NUM register (see Table 48) contains a lot-specific serial number. Table 47. PROD_ID (Page 0, Base Address = 0x7E) Bits [15:0] Description (Default = 0x4065) Product identification = 0x4065 (16,485) Table 48. SERIAL_NUM (Page 4, Base Address = 0x20) Bits [15:0] Rev. H | Page 19 of 32 Description Lot specific serial number ADIS16485 Data Sheet DIGITAL SIGNAL PROCESSING GYROSCOPES/ACCELEROMETERS AVERAGING/DECIMATION FILTER Figure 20 provides a signal flow diagram for all the components and settings that influence the frequency response for the accelerometers and gyroscopes. The sample rate for each accelerometer and gyroscope is 9.84 kHz. Each sensor has its own averaging/decimation filter stage that reduces the update rate to 2.46 kSPS. When using the external sync clock option (FNCTIO_CTRL[7:4], see Table 89), the input clock drives a 4-sample burst at a sample rate of 9.84 kSPS, which feeds into the 4× averaging/decimation filter. This results in a data rate that is equal to the input clock frequency. The DEC_RATE register (see Table 49) provides user control for the final filter stage (see Figure 20), which averages and decimates the accelerometers, gyroscopes, delta angle, and delta velocity data. The output sample rate is equal to 2460/(DEC_RATE + 1). When using the external sync clock option (FNCTIO_CTRL[7:4], see Table 89), 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). Table 49. DEC_RATE (Page 3, Base Address = 0x0C) Bits [15:11] [10:0] Description (Default = 0x0000) Don’t care Decimation rate, binary format, maximum = 2047, see Figure 20 for impact on sample rate 2.46kHz, fs MEMS SENSOR 1 4 330Hz GYROSCOPE 2-POLE: 404Hz, 757Hz ACCELEROMETER 1-POLE: 330Hz INTERNAL CLOCK 9.84kHz fs 4 FIR FILTER BANK ÷4 4× AVERAGE DECIMATION FILTER 1 D D ÷D SELECTABLE AVERAGE/DECIMATION FILTER FIR FILTER BANK D = DEC_RATE[10:0] + 1 FILTR_BNK_0 FILTR_BNK_1 NOTES 1. WHEN FNCTIO_CTRL[7] = 1, EACH CLOCK PULSE ON THE DESIGNATED DIOx LINE (FNCTIO_CTRL[5:4]) STARTS A 4-SAMPLE BURST, AT A SAMPLE RATE OF 9.84kHz. THESE FOUR SAMPLES FEED INTO THE 4x AVERAGE/DECIMATION FILTER, WHICH PRODUCES A DATA RATE THAT IS EQUAL TO THE INPUT CLOCK FREQUENCY. Figure 20. Sampling and Frequency Response Signal Flow Rev. H | Page 20 of 32 10666-019 DIOx OPTIONAL INPUT CLOCK FNCTIO_CTRL[7] = 1 fs < 2400Hz Data Sheet ADIS16485 FIR FILTER BANKS Table 52. Filter Bank A Memory Map, FIR_COEF_Axxx The ADIS16485 provides four configurable, 120-tap FIR filter banks. Each coefficient is 16 bits wide and occupies its own register location with each page. When designing a FIR filter for these banks, use a sample rate of 2.46 kHz and scale the coefficients so that their sum equals 32,768. For filter designs that have less than 120 taps, load the coefficients into the lower portion of the filter and start with Coefficient 1. Make sure that all unused taps are equal to zero, so that they do not add phase delay to the response. The FILTR_BNK_x registers provide three bits per sensor, which configure the filter bank (A, B, C, D) and turn filtering on and off. For example, turn to Page 3 (DIN = 0x8003), then write 0x002F to FILTR_BNK_0 (DIN = 0x962F, DIN = 0x9700) to set the x-axis gyroscope to use the FIR filter in Bank D, to set the y-axis gyroscope to use the FIR filter in Bank B, and to enable these FIR filters in both x- and y-axis gyroscopes. Note that the filter settings update after writing to the upper byte; therefore, always configure the lower byte first. In cases that require configuration to only the lower byte of either FILTR_BNK_0 or FILTR_BNK_1, complete the process by writing 0x00 to the upper byte. Page 5 5 5 5 5 PAGE_ID 0x05 0x05 0x05 0x05 0x05 Address 0x00 0x02 to 0x07 0x08 0x0A 0x0C to 0x7C 5 6 6 6 6 6 0x05 0x06 0x06 0x06 0x06 0x06 0x7E 0x00 0x02 to 0x07 0x08 0x0A 0x0C to 0x7C 6 0x06 0x7E Table 50. FILTR_BNK_0 (Page 3, Base Address = 0x16) Bits 15 14 [13:12] 11 [10:9] 8 [7:6] 5 [4:3] 2 [1:0] Description (Default = 0x0000) Don’t care Y-axis accelerometer filter enable (1 = enabled) Y-axis accelerometer filter bank selection: 00 = Bank A, 01 = Bank B, 10 = Bank C, 11 = Bank D X-axis accelerometer filter enable (1 = enabled) X-axis accelerometer filter bank selection: 00 = Bank A, 01 = Bank B, 10 = Bank C, 11 = Bank D Z-axis gyroscope filter enable (1 = enabled) Z-axis gyroscope filter bank selection: 00 = Bank A, 01 = Bank B, 10 = Bank C, 11 = Bank D Y-axis gyroscope filter enable (1 = enabled) Y-axis gyroscope filter bank selection: 00 = Bank A, 01 = Bank B, 10 = Bank C, 11 = Bank D X-axis gyroscope filter enable (1 = enabled) X-axis gyroscope filter bank selection: 00 = Bank A, 01 = Bank B, 10 = Bank C, 11 = Bank D Table 51. FILTR_BNK_1 (Page 3, Base Address = 0x18) Bits [15:3] 2 [1:0] Description (Default = 0x0000) Don’t care Z-axis accelerometer filter enable (1 = enabled) Z-axis accelerometer filter bank selection: 00 = Bank A, 01 = Bank B, 10 = Bank C, 11 = Bank D Filter Memory Organization Each filter bank uses two pages of the user register structure. See Table 52, Table 53, Table 54 and Table 55 for the register addresses in each filter bank. Register PAGE_ID Not used FIR_COEF_A000 FIR_COEF_A001 FIR_COEF_A002 to FIR_COEF_A058 FIR_COEF_A059 PAGE_ID Not used FIR_COEF_A060 FIR_COEF_A061 FIR_COEF_A062 to FIR_COEF_A118 FIR_COEF_A119 Table 53. Filter Bank B Memory Map, FIR_COEF_Bxxx Page 7 7 7 7 7 PAGE_ID 0x07 0x07 0x07 0x07 0x07 Address 0x00 0x02 to 0x07 0x08 0x0A 0x0C to 0x7C 7 8 8 8 8 8 0x07 0x08 0x08 0x08 0x08 0x08 0x7E 0x00 0x02 to 0x07 0x08 0x0A 0x0C to 0x7C 8 0x08 0x7E Register PAGE_ID Not used FIR_COEF_B000 FIR_COEF_B001 FIR_COEF_B002 to FIR_COEF_B058 FIR_COEF_B059 PAGE_ID Not used FIR_COEF_B060 FIR_COEF_B061 FIR_COEF_B062 to FIR_COEF_B118 FIR_COEF_B119 Table 54. Filter Bank C Memory Map, FIR_COEF_Cxxx Page 9 9 9 9 9 PAGE_ID 0x09 0x09 0x09 0x09 0x09 Address 0x00 0x02 to 0x07 0x08 0x0A 0x0C to 0x7C 9 10 10 10 10 10 0x09 0x0A 0x0A 0x0A 0x0A 0x0A 0x7E 0x00 0x02 to 0x07 0x08 0x0A 0x0C to 0x7C 10 0x0A 0x7E Rev. H | Page 21 of 32 Register PAGE_ID Not used FIR_COEF_C000 FIR_COEF_C001 FIR_COEF_C002 to FIR_COEF_C058 FIR_COEF_C059 PAGE_ID Not used FIR_COEF_C060 FIR_COEF_C061 FIR_COEF_C062 to FIR_COEF_C118 FIR_COEF_C119 ADIS16485 Data Sheet Table 55. Filter Bank D Memory Map, FIR_COEF_Dxxx Table 56. FIR Filter Descriptions, Default Configuration Page 11 11 11 11 11 PAGE_ID 0x0B 0x0B 0x0B 0x0B 0x0B Address 0x00 0x02 to 0x07 0x08 0x0A 0x0C to 0x7C FIR Filter Bank A B C D 11 12 12 12 12 12 0x0B 0x0C 0x0C 0x0C 0x0C 0x0C 0x7E 0x00 0x02 to 0x07 0x08 0x0A 0x0C to 0x7C 12 0x0C 0x7E Register PAGE_ID Not used FIR_COEF_D000 FIR_COEF_D001 FIR_COEF_D002 to FIR_COEF_D058 FIR_COEF_D059 PAGE_ID Not used FIR_COEF_D060 FIR_COEF_D061 FIR_COEF_D062 to FIR_COEF_D118 FIR_COEF_D119 Taps 120 120 32 32 −3 dB Frequency (Hz) 310 55 275 63 0 –10 MAGNITUDE (dB) –20 B D NO FIR FILTERING C A –30 –40 –50 –60 –70 –80 Default Filter Performance Rev. H | Page 22 of 32 –100 0 200 400 600 800 1000 FREQUENCY (Hz) Figure 21. FIR Filter Frequency Response Curves 1200 10666-020 –90 The FIR filter banks have factory programmed filter designs. They are all low-pass filters that have unity dc gain. Table 56 provides a summary of each filter design, and Figure 21 shows the frequency response characteristics. The phase delay is equal to ½ of the total number of taps. Data Sheet ADIS16485 CALIBRATION The ADIS16485 factory calibration produces correction formulas for the gyroscopes and the accelerometers and then programs them into the flash memory. In addition, there are a series of user-configurable calibration registers for in-system tuning. Bias Null Command GYROSCOPES The user calibration for the gyroscopes includes registers for adjusting bias and sensitivity, as shown in Figure 22. 1 + X_GYRO_SCALE FACTORY CALIBRATION AND FILTERING XG_BIAS_HIGH X_GYRO_OUT X_GYRO_LOW 10666-021 X-AXIS GYRO XG_BIAS_LOW Figure 22. User Calibration Signal Path, Gyroscopes Manual Bias Correction The xG_BIAS_HIGH registers (see Table 57, Table 58, and Table 59) and xG_BIAS_LOW registers (see Table 60, Table 61, and Table 62) provide a bias adjustment function for the output of each gyroscope sensor. Table 57. XG_BIAS_HIGH (Page 2, Base Address = 0x12) Bits [15:0] Description (Default = 0x0000) X-axis gyroscope offset correction, upper word; twos complement, 0°/sec = 0x0000, 1 LSB = 0.02°/sec Table 58. YG_BIAS_HIGH (Page 2, Base Address = 0x16) Bits [15:0] Description (Default = 0x0000) Y-axis gyroscope offset correction, upper word; twos complement, 0°/sec = 0x0000, 1 LSB = 0.02°/sec Table 59. ZG_BIAS_HIGH (Page 2, Base Address = 0x1A) Bits [15:0] Description (Default = 0x0000) Z-axis gyroscope offset correction, upper word; twos complement, 0°/sec = 0x0000, 1 LSB = 0.02°/sec Table 60. XG_BIAS_LOW (Page 2, Base Address = 0x10) Bits [15:0] Description (Default = 0x0000) X-axis gyroscope offset correction, lower word; twos complement, 0°/sec = 0x0000, 1 LSB = 0.02°/sec ÷ 216 = ~0.000000305°/sec Table 61. YG_BIAS_LOW (Page 2, Base Address = 0x14) Bits [15:0] Description (Default = 0x0000) Y-axis gyroscope offset correction, lower word; twos complement, 0°/sec = 0x0000, 1 LSB = 0.02°/sec ÷ 216 = ~0.000000305°/sec Table 62. ZG_BIAS_LOW (Page 2, Base Address = 0x18) Bits [15:0] Description (Default = 0x0000) Z-axis gyroscope offset correction, lower word; twos complement, 0°/sec = 0x0000, 1 LSB = 0.02°/sec ÷ 216 = ~0.000000305°/sec The continuous bias estimator (CBE) accumulates and averages data in a 64-sample FIFO. The average time (tA) for the bias estimates relies on the sample time base setting in NULL_CNFG[3:0] (see Table 63). Users can load the correction factors of the CBE into the gyroscope offset correction registers (see Table 57, Table 58, Table 59, Table 60, Table 61, and Table 62) using the bias null command in GLOB_CMD[0] (see Table 86). NULL_CNFG[13:8] provide on/off controls for the sensors that update when issuing a bias null command. The factory default configuration for NULL_CNFG enables the bias null command for the gyroscopes, disables the bias null command for the accelerometers, and establishes the average time to ~26.64 seconds. For best results, make sure the ADIS16485 is stationary for this entire time. Table 63. NULL_CNFG (Page 3, Base Address = 0x0E) Bits [15:14] 13 12 11 10 9 8 [7:4] [3:0] Description (Default = 0x070A) Not used Z-axis acceleration bias correction enable (1 = enabled) Y-axis acceleration bias correction enable (1 = enabled) X-axis acceleration bias correction enable (1 = enabled) Z-axis gyroscope bias correction enable (1 = enabled) Y-axis gyroscope bias correction enable (1 = enabled) X-axis gyroscope bias correction enable (1 = enabled) Not used Time base control (TBC), range: 0 to 13 (default = 10); tB = 2TBC/2460, time base, tA = 64 × tB, average time Turn to Page 3 (DIN = 0x8003) and set GLOB_CMD[0] = 1 (DIN = 0x8201, then DIN = 0x8300) to update the user offset registers with the correction factors of the CBE. Manual Sensitivity Correction The x_GYRO_SCALE registers enable sensitivity adjustment (see Table 64, Table 65, and Table 66). Table 64. X_GYRO_SCALE (Page 2, Base Address = 0x04) Bits [15:0] Description (Default = 0x0000) X-axis gyroscope scale correction; twos complement, 0x0000 = unity gain, 1 LSB = 1 ÷ 215 = ~0.003052% Table 65. Y_GYRO_SCALE (Page 2, Base Address = 0x06) Bits [15:0] Description (Default = 0x0000) Y-axis gyroscope scale correction; twos complement, 0x0000 = unity gain, 1 LSB = 1 ÷ 215 = ~0.003052% Table 66. Z_GYRO_SCALE (Page 2, Base Address = 0x08) Bits [15:0] Rev. H | Page 23 of 32 Description (Default = 0x0000) Z-axis gyroscope scale correction; twos complement, 0x0000 = unity gain, 1 LSB = 1 ÷ 215 = ~0.003052% ADIS16485 Data Sheet Linear Acceleration on Effect on Gyroscope Bias MEMS gyroscopes typically have a bias response to linear acceleration that is normal to their axes of rotation. The ADIS16485 offers an optional compensation function for this effect; the factory default setting (0x00C0) for the CONFIG register enables this function. To turn it off, turn to Page 3 (DIN = 0x8003) and set CONFIG[7] = 0 (DIN = 0x8A20, DIN = 0x8B00). Note that this also keeps the point of percussion alignment function enabled. Table 69. YA_BIAS_HIGH (Page 2, Base Address = 0x22) Bits [15:0] Table 70. ZA_BIAS_HIGH (Page 2, Base Address = 0x26) Bits [15:0] Table 67. CONFIG (Page 3, Base Address = 0x0A) Bits [15:8] 7 6 [5:2] 1 0 Bits [15:0] Bits [15:0] 1 + X_ACCL_SCALE X_ACCL_LOW XA_BIAS_LOW Figure 23. User Calibration Signal Path, Gyroscopes The xA_BIAS_HIGH (see Table 68, Table 69, and Table 70) and xA_BIAS_LOW (see Table 71, Table 72, and Table 73) registers provide a bias adjustment function for the output of each accelerometer sensor. The xA_BIAS_HIGH registers use the same format as x_ACCL_OUT registers. The xA_BIAS_LOW registers use the same format as x_ACCL_LOW registers. Table 68. XA_BIAS_HIGH (Page 2, Base Address = 0x1E) Description (Default = 0x0000) X-axis accelerometer offset correction, high word; twos complement, 0 g = 0x0000, 1 LSB = 0.25 mg Table 73. ZA_BIAS_LOW (Page 2, Base Address = 0x24) Bits [15:0] Description (Default = 0x0000) Z-axis accelerometer offset correction, low word; twos complement, 0 g = 0x0000, 1 LSB = 0.25 mg ÷ 216 = ~0.000003815 mg The x_ACCL_SCALE registers enable sensitivity adjustment (see Table 74, Table 75, Table 76). Table 74. X_ACCL_SCALE (Page 2, Base Address = 0x0A) Manual Bias Correction Bits [15:0] Description (Default = 0x0000) Y-axis accelerometer offset correction, low word; twos complement, 0 g = 0x0000, 1 LSB = 0.25 mg ÷ 216 = ~0.000003815 mg Manual Sensitivity Correction 10666-022 XA_BIAS_HIGH X_ACCL_OUT Description (Default = 0x0000) X-axis accelerometer offset correction, low word; twos complement, 0 g = 0x0000, 1 LSB = 0.25 mg ÷ 216 = ~0.000003815 mg Table 72. YA_BIAS_LOW (Page 2, Base Address = 0x20) The user calibration for the accelerometers includes registers for adjusting bias and sensitivity, as shown in Figure 23. FACTORY CALIBRATION AND FILTERING Description (Default = 0x0000) Z-axis accelerometer offset correction, high word; twos complement, 0 g = 0x0000, 1 LSB = 0.25 mg Table 71. XA_BIAS_LOW (Page 2, Base Address = 0x1C) Description (Default = 0x00C0) Not used Linear-g compensation for gyroscopes (1 = enabled) Point of percussion alignment (1 = enabled) Not used Real-time clock, daylight savings time (1: enabled, 0: disabled) Real-time clock control (1: relative/elapsed timer mode, 0: calendar mode) ACCELEROMETERS X-AXIS ACCL Description (Default = 0x0000) Y-axis accelerometer offset correction, high word; twos complement, 0 g = 0x0000, 1 LSB = 0.25 mg Bits [15:0] Description (Default = 0x0000) X-axis accelerometer scale correction; twos complement, 0x0000 = unity gain, 1 LSB = 1 ÷ 215 = ~0.003052% Table 75. Y_ACCL_SCALE (Page 2, Base Address = 0x0C) Bits [15:0] Description (Default = 0x0000) Y-axis accelerometer scale correction; twos complement, 0x0000 = unity gain, 1 LSB = 1 ÷ 215 = ~0.003052% Table 76. Z_ACCL_SCALE (Page 2, Base Address = 0x0E) Bits [15:0] Rev. H | Page 24 of 32 Description (Default = 0x0000) Z-axis accelerometer scale correction; twos complement, 0x0000 = unity gain, 1 LSB = 1 ÷ 215 = ~0.003052% Data Sheet ADIS16485 RESTORING FACTORY CALIBRATION Turn to Page 3 (DIN = 0x8003) and set GLOB_CMD[6] = 1 (DIN = 0x8240, DIN = 0x8300) to execute the factory calibration restore function. This function resets each user calibration register to zero, resets all sensor data to 0, and automatically updates the flash memory within 900 ms. See Table 86 for more information on GLOB_CMD. PIN 23 POINT OF PERCUSSION ALIGNMENT REFERENCE POINT. SEE CONFIG[6]. POINT OF PERCUSSION ALIGNMENT CONFIG[6] offers a point of percussion alignment function that maps the accelerometer sensors to the corner of the package identified in Figure 24. To activate this feature, turn to Page 3 (DIN = 0x8003), then set CONFIG[6] = 1 (DIN = 0x8A40, DIN = 0x8B00). See Table 67 for more information on the CONFIG register. Rev. H | Page 25 of 32 Figure 24. Point of Percussion Reference Point 10666-023 PIN 1 ADIS16485 Data Sheet ALARMS Each sensor has an independent alarm function that provides controls for alarm magnitude, polarity, and enabling a dynamic rate-of-change option. The ALM_STS register (see Table 43) contains the alarm output flags and the FNCTIO_CTRL register (see Table 89) provides an option for configuring one of the digital I/O lines as an alarm indicator. Table 83. ALM_CNFG_0 (Page 3, Base Address = 0x20) Bits 15 14 13 STATIC ALARM USE The static alarm setting compares the output of each sensor with the trigger settings in the xx_ALM_MAGN registers (see Table 77, Table 78, Table 79, Table 80, Table 81, and Table 82) of that sensor. The polarity controls for each alarm are in the ALM_CNFG_x registers (see Table 83 and Table 84) and establish the relationship for the condition that causes the corresponding alarm flag to be active. For example, when ALM_CNFG_0[13] = 1, the alarm flag for the x-axis accelerometer (ALM_STS[3], see Table 43) becomes active (equal to 1) when X_ACCL_OUT is greater than XA_ALM_MAGN. 12 11 10 9 8 7 6 5 DYNAMIC ALARM USE The dynamic alarm setting provides the option to compare the change in each sensor output over a period of 48.7 ms with the xx_ALM_MAGN register that sensor. Table 77. XG_ALM_MAGN (Page 3, Base Address = 0x28) Bits [15:0] Description (Default = 0x0000) X-axis gyroscope alarm threshold settings; twos complement, 0°/sec = 0x0000, 1 LSB = 0.02°/sec Table 78. YG_ALM_MAGN (Page 3, Base Address = 0x2A) Bits [15:0] Description (Default = 0x0000) Y-axis gyroscope alarm threshold settings; twos complement, 0°/sec = 0x0000, 1 LSB = 0.02°/sec Table 79. ZG_ALM_MAGN (Page 3, Base Address = 0x2C) Bits [15:0] Description (Default = 0x0000) Z-axis gyroscope alarm threshold settings; twos complement, 0°/sec = 0x0000, 1 LSB = 0.02°/sec Table 80. XA_ALM_MAGN (Page 3, Base Address = 0x2E) Bits [15:0] Description (Default = 0x0000) X-axis accelerometer alarm threshold settings; twos complement, 0 g = 0x0000, 1 LSB = 0.25 mg 4 3 2 1 0 Description (Default = 0x0000) X-axis accelerometer alarm (1 = enabled) Not used X-axis accelerometer alarm polarity 1 = active when X_ACCL_OUT > XA_ALM_MAGN 0 = active when X_ACCL_OUT > XA_ALM_MAGN X-axis accelerometer dynamic enable (1 = enabled) Z-axis gyroscope alarm (1 = enabled) Not used Z-axis gyroscope alarm polarity 1 = active when Z_GYRO_OUT > ZG_ALM_MAGN 0 = active when Z_GYRO_OUT > ZG_ALM_MAGN Z-axis gyroscope dynamic enable (1 = enabled) Y-axis gyroscope alarm (1 = enabled) Not used Y-axis gyroscope alarm polarity 1 = active when Y_GYRO_OUT > YG_ALM_MAGN 0 = active when Y_GYRO_OUT > YG_ALM_MAGN Y-axis gyroscope dynamic enable (1 = enabled) X-axis gyroscope alarm (1 = enabled) Not used X-axis gyroscope alarm polarity 1 = active when X_GYRO_OUT > XG_ALM_MAGN 0 = active when X_GYRO_OUT > XG_ALM_MAGN X-axis gyroscope dynamic enable (1 = enabled) Table 84. ALM_CNFG_1 (Page 3, Base Address = 0x22) Bits [15:8] 7 6 5 4 3 2 1 Description (Default = 0x0000) Don’t care Z-axis accelerometer alarm (1 = enabled) Not used Z-axis accelerometer alarm polarity 1 = active when Z_ACCL_OUT > ZA_ALM_MAGN 0 = active when Z_ACCL_OUT > ZA_ALM_MAGN Z-axis accelerometer dynamic enable (1 = enabled) Y-axis accelerometer alarm (1 = enabled) Not used Y-axis accelerometer alarm polarity 1 = active when Y_ACCL_OUT > YA_ALM_MAGN 0 = active when Y_ACCL_OUT > YA_ALM_MAGN Y-axis accelerometer dynamic enable (1 = enabled) Table 81. YA_ALM_MAGN (Page 3, Base Address = 0x30) 0 Bits [15:0] Alarm Example Description (Default = 0x0000) Y-axis accelerometer alarm threshold settings; twos complement, 0 g = 0x0000, 1 LSB = 0.25 mg Table 82. ZA_ALM_MAGN (Page 3, Base Address = 0x32) Bits [15:0] Description (Default = 0x0000) Z-axis accelerometer alarm threshold settings; twos complement, 0 g = 0x0000, 1 LSB = 0.25 mg Table 85 offers an alarm configuration example, which sets the z-axis gyroscope alarm to trip when Z_GYRO_OUT > 131.1°/sec (0x199B). Table 85. Alarm Configuration Example DIN 0xAC9B, 0xAD19 0xA000, 0xA10A Rev. H | Page 26 of 32 Description Set ZG_ALM_MAGN = 0x199B Set ALM_CNFG_0 = 0x0A00 Data Sheet ADIS16485 SYSTEM CONTROLS The ADIS16485 provides a number of system level controls for managing its operation, which include reset, self test, calibration, memory management, and I/O configuration. GLOBAL COMMANDS The GLOB_CMD register (see Table 86) provides trigger bits for several operations. Write 1 to the appropriate bit in GLOB_CMD to start a function. After the function completes, the bit restores to 0. Description Not used Software reset Factory calibration restore Not used Flash memory update Flash memory test Self test Bias null The data retention of the flash memory depends on the temperature and the number of write cycles. Figure 25 characterizes the dependence on temperature, and the FLSHCNT_LOW and FLSHCNT_HIGH registers (see Table 87 and Table 88) provide a running count of flash write cycles. The flash updates every time GLOB_CMD[6], GLOB_CMD[3], or GLOB_CMD[0] is set to 1. Table 87. FLSHCNT_LOW (Page 2, Base Address = 0x7C) Table 86. GLOB_CMD (Page 3, Base Address = 0x02) Bits [15:8] 7 6 [5:4] 3 2 1 0 MEMORY MANAGEMENT Execution Time Not applicable 120 ms 75 ms Not applicable 375 ms 50 ms 12 ms See Table 63 Bits [15:0] Description Binary counter; number of flash updates, lower word Table 88. FLSHCNT_HIGH (Page 2, Base Address = 0x7E) Bits [15:0] Description Binary counter; number of flash updates, upper word 600 Turn to Page 3 (DIN = 0x8003) and then set GLOB_CMD[7] = 1 (DIN = 0x8280, DIN = 0x8300) to reset the operation, which removes all data, initializes all registers from their flash settings, and starts data collection. This function provides a firmware alternative to the RST pin (see Table 6, Pin 8). RETENTION (Years) Software Reset Automatic Self Test 300 Measure the output on each sensor. Activate the self test on each sensor. Measure the output on each sensor. Deactivate the self test on each sensor. Calculate the difference with the self test on and off. Compare the difference with the internal pass/fail criteria. Report the pass/fail results for each sensor in DIAG_STS. After waiting 12 ms for this test to complete, turn to Page 0 (DIN = 0x8000) and read DIAG_STS using DIN = 0x0A00. Note that using an external clock can extend this time. When using an external clock of 100 Hz, this time extends to 35 ms. Note that 100 Hz is too slow for optimal sensor performance. 0 30 40 55 70 85 100 125 JUNCTION TEMPERATURE (°C) 135 150 10666-024 150 Turn to Page 3 (DIN = 0x8003) and then set GLOB_CMD[1] = 1 (DIN = 0x8202, then DIN = 0x8300) to run an automatic, self test routine, which executes the following steps: 1. 2. 3. 4. 5. 6. 7. 450 Figure 25. Flash Memory Retention Flash Memory Test Turn to Page 3 (DIN = 0x8003), and then set GLOB_CMD[2] = 1 (DIN = 0x8204, DIN = 0x8300) to run a checksum test of the internal flash memory, which compares a factory programmed value with the current sum of the same memory locations. The result of this test loads into SYS_E_FLAG[6]. Turn to Page 0 (DIN = 0x8000) and use DIN = 0x0800 to read SYS_E_FLAG. Rev. H | Page 27 of 32 ADIS16485 Data Sheet GENERAL-PURPOSE I/O General-Purpose I/O Control There are four general-purpose I/O pins: DIO1, DIO2, DIO3, and DIO4. The FNCTIO_CTRL register controls the basic function of each I/O pin. Each I/O pin only supports one function at a time. In cases where a single pin has two different assignments, the enable bit for the lower priority function automatically resets to zero and is disabled. The priority is (1) data-ready, (2) sync clock input, (3) alarm indicator, and (4) general-purpose, where 1 identifies the highest priority and 4 indicates the lowest priority. When FNCTIO_CTRL does not configure a DIOx pin, GPIO_CTRL provides register controls for general-purpose use of the pin. GPIO_CTRL[3:0] provides input/output assignment controls for each pin. When the DIOx pins are inputs, monitor their levels by reading GPIO_CTRL[7:4]. When the DIOx pins are used as outputs, set their levels by writing to GPIO_CTRL[7:4]. For example, use the following sequence to set DIO1 and DIO3 as high and low output pins, respectively, and set DIO2 and DIO4 as input pins. Turn to Page 3 (DIN = 0x8003) and set GPIO_CTRL[7:0] = 0x15 (DIN = 0x8815, then DIN = 0x8900). Table 89. FNCTIO_CTRL (Page 3, Base Address = 0x06) Bits [15:12] 11 10 [9:8] 7 6 [5:4] 3 2 [1:0] Description (Default = 0x000D) Not used Alarm indicator: 1 = enabled, 0 = disabled Alarm indicator polarity: 1 = positive, 0 = negative Alarm indicator line selection: 00 = DIO1, 01 = DIO2, 10 = DIO3, 11 = DIO4 Sync clock input enable: 1 = enabled, 0 = disabled Sync clock input polarity: 1 = rising edge, 0 = falling edge Sync clock input line selection: 00 = DIO1, 01 = DIO2, 10 = DIO3, 11 = DIO4 Data-ready enable: 1 = enabled, 0 = disabled Data-ready polarity: 1 = positive, 0 = negative Data-ready line selection: 00 = DIO1, 01 = DIO2, 10 = DIO3, 11 = DIO4 Table 90. GPIO_CTRL (Page 3, Base Address = 0x08) Bits [15:8] 7 6 5 4 3 2 1 0 Data-Ready Indicator FNCTIO_CTRL[3:0] provide some configuration options for using one of the DIOx lines as a data-ready indicator signal, which can drive the interrupt control line of a processor. The factory default assigns DIO2 as a positive polarity, data-ready signal. Use the following sequence to change this assignment to DIO1 with a negative polarity: turn to Page 3 (DIN = 0x8003) and set FNCTIO_CTRL[3:0] = 1000 (DIN = 0x8608, then DIN = 0x8700). The timing jitter on the data-ready signal is ±1.4 µs. Input Sync/Clock Control FNCTIO_CTRL[7:4] provide some configuration options for using one of the DIOx lines as an input synchronization signal for sampling inertial sensor data. For example, use the following sequence to establish DIO4 as a positive polarity, input clock pin and keep the factory default setting for the data-ready function: turn to Page 3 (DIN = 0x8003) and set FNCTIO_CTRL[7:0] = 0xFD (DIN = 0x86FD, then DIN = 0x8700). Note that this command also disables the internal sampling clock, and no data sampling takes place without the input clock signal. When selecting a clock input frequency, consider the 330 Hz sensor bandwidth, because under sampling the sensors can degrade noise and stability performance. 1 Description (Default = 0x00X0)1 Don’t care General-Purpose I/O Line 4 (DIO4) data level General-Purpose I/O Line 3 (DIO3) data level General-Purpose I/O Line 2 (DIO2) data level General-Purpose I/O Line 1 (DIO1) data level General-Purpose I/O Line 4 (DIO4) direction control (1 = output, 0 = input) General-Purpose I/O Line 3 (DIO3) direction control (1 = output, 0 = input) General-Purpose I/O Line 2 (DIO2) direction control (1 = output, 0 = input) General-Purpose I/O Line 1 (DIO1) direction control (1 = output, 0 = input) The GPIO_CTRL register, Bits[7:4], reflect the levels on the DIOx pins and do not have a default setting. POWER MANAGEMENT The SLP_CNT register (see Table 91) provides controls for both power-down mode and sleep mode. The trade-off between powerdown mode and sleep mode is between idle power and recovery time. Power-down mode offers the best idle power consumption but requires the most time to recover. Also, all volatile settings are lost during power-down but are preserved during sleep mode. For timed sleep mode, turn to Page 3 (DIN = 0x8003), write the amount of sleep time to SLP_CNT[7:0] and then, set SLP_CNT[8] = 1 (DIN = 0x9101) to start the sleep period. For a timed power-down period, change the last command to set SLP_CNT[9] = 1 (DIN = 0x9102). To power down or sleep for an indefinite period, set SLP_CNT[7:0] = 0x00 first, then set either SLP_CNT[8] or SLP_CNT[9] to 1. Note that the command takes effect when the CS line goes high. To awaken the device from sleep or power-down mode, use one of the following options to restore normal operation: • Assert CS from high to low. • Pulse RST low, then high again. Cycle the power. • For example, set SLP_CNT[7:0] = 0x64 (DIN = 0x9064), then set SLP_CNT[8] = 1 (DIN = 0x9101) to start a sleep period of 100 seconds. Rev. H | Page 28 of 32 Data Sheet ADIS16485 Table 91. SLP_CNT (Page 3, Base Address = 0x10) Bits [15:10] 9 8 [7:0] Description Not used Power-down mode Normal sleep mode Programmable time bits; 1 sec/LSB; 0x00 = indefinite If the sleep mode and power-down mode bits are both set high, the normal sleep mode (SLP_CNT[8]) bit takes precedence. General-Purpose Registers The USER_SCR_x registers (see Table 92, Table 93, Table 94, and Table 95) provide four 16-bit registers for storing data. Table 92. USER_SCR_1 (Page 2, Base Address = 0x74) Bits [15:0] Description User-defined Table 93. USER_SCR_2 (Page 2, Base Address = 0x76) Bits [15:0] Description User-defined Bits [15:14] [13:8] [7:6] [5:0] Description User-defined Table 95. USER_SCR_4 (Page 2, Base Address = 0x7A) Bits [15:0] Write the current time to each time data register after setting CONFIG[0] = 1 (DIN = 0x8003, DIN = 0x8A01). Note that CONFIG[1] provides a bit for managing daylight savings time. After the CONFIG and TIME_xx_OUT registers are configured, set GLOB_CMD[3] = 1 (DIN = 0x8003, DIN = 0x8208, DIN = 0x8300) to back up these settings up in flash, and use a separate 3.3 V source to supply power to the VDDRTC function. Note that access to time data in the TIME_xx_OUT registers requires normal operation (VDD = 3.3 V and full startup), but the timer function only requires that VDDRTC = 3.3 V when the rest of the ADIS16485 is turned off. Table 96. TIME_MS_OUT (Page 0, Base Address = 0x78) Table 94. USER_SCR_3 (Page 2, Base Address = 0x78) Bits [15:0] The updates to the timer do not become active until there is a successful write to the TIME_ YM_OUT[14:8] byte. The realtime clock registers reflect the newly updated values only after the next seconds tick of the clock that follows the write to TIME_YM_OUT[14:8] (year). Writing to TIME_YM_OUT[14:8] activates all timing values; therefore, always write to this location last when updating the timer, even if the year information does not require updating. Description User-defined Description Not used Minutes, binary data, range = 0 to 59 Not used Seconds, binary data, range = 0 to 59 Table 97. TIME_DH_OUT (Page 0, Base Address = 0x7A) Real-Time Clock Configuration/Data The VDDRTC power supply pin (see Table 6, Pin 23) provides a separate supply for the real-time clock (RTC) function. This enables the RTC to keep track of time, even when the main supply (VDD) is off. Configure the RTC function by selecting one of two modes in CONFIG[0] (see Table 67). The real-time clock data is available in the TIME_MS_OUT register (see Table 96), TIME_DH_OUT register (see Table 97), and TIME_YM_OUT register (see Table 98). When using the elapsed timer mode, the time data registers start at 0x0000 when the device starts up (or resets) and begin keeping time in a manner that is similar to a stopwatch. When using the clock/calendar mode, write the current time to the real-time registers in the following sequence: seconds (TIME_MS_OUT[5:0]), minutes (TIME_ MS_OUT[13:8]), hours (TIME_DH_OUT[5:0]), day (TIME_DH_OUT[12:8]), month (TIME_YM_OUT[3:0]), and year (TIME_YM_OUT[14:8]). Bits [15:13] [12:8] [7:6] [5:0] Description Not used Day, binary data, range = 1 to 31 Not used Hours, binary data, range = 0 to 23 Table 98. TIME_YM_OUT (Page 0, Base Address = 0x7C) Bits [15] [14:8] [7:4] [3:0] Rev. H | Page 29 of 32 Description Not used Year, binary data, range = 0 to 99, relative to 2000 A.D. Not used Month, binary data, range = 1 to 12 ADIS16485 Data Sheet APPLICATIONS INFORMATION MOUNTING TIPS 39.600 BSC 19.800 BSC For best performance, follow these simple rules when installing the ADIS16485 into a system. 0.560 BSC 2× ALIGNMENT HOLES FOR MATING SOCKET 5 BSC 5 BSC NOTES 1. ALL DIMENSIONS IN mm UNITS. 2. THE CONNECTOR FACES DOWN AND ARE NOT VISIBLE FROM THIS VIEW. 10666-027 These three rules help prevent nonuniform force profiles, which can warp the package and introduce bias errors in the sensors. Figure 26 provides an example that leverages washers to set the package off the mounting surface and uses 2.85 mm pass-through holes and backside washers/nuts for attachment. Figure 27 and Figure 28 provide some details from mounting hole and connector alignment pin drill locations. For more information on mounting the ADIS16485, see the AN-1295 Application Note. ADIS16485AMLZ OUTLINE 1.642 BSC Figure 27. Suggested PCB Layout Pattern, Connector Down 0.4334 [11.0] 0.019685 [0.5000] (TYP) MOUNTING SCREWS M2 × 0.4mm, 4× 0.0240 [0.610] 0.054 [1.37] 0.0394 [1.00] 0.1800 [4.57] WASHERS (OPTIONAL) M2, 4× ADIS16488A SPACERS/WASHERS SUGGESTED, 4× 0.022± DIA (TYP) NONPLATED THROUGH HOLE 2× PCB 0.0394 [1.00] 0.022 DIA THROUGH HOLE (TYP) NONPLATED THROUGH HOLE Figure 28. Suggested Layout and Mechanical Design when Using Samtec P/N CLM-112-02-G-D-A for the Mating Connector MATING CONNECTOR CLM-112-02 PASS-THROUGH HOLES DIAMETER ≥ 2.85mm NUTS M2 × 0.4mm, 4× 10666-133 WASHERS (OPTIONAL) M2, 4× Figure 26. Mounting Example Rev. H | Page 30 of 32 10666-028 3. 42.600 2. Eliminate opportunity for translational force (x-axis and y-axis direction; see Figure 6. Isolate mounting force to the four corners, on the part of the package surface that surrounds the mounting holes. Use uniform mounting forces on all four corners. The suggested torque setting is 40 inch-ounces (0.285 N-m). 21.300 BSC 1. PASS-THROUGH HOLE FOR MOUNTING SCREWS DIAMETER OF THE HOLE MUST ACCOMMODATE DIMENSIONAL TOLERANCE BETWEEN THE CONNECTOR AND HOLES. Data Sheet ADIS16485 EVALUATION TOOLS T VDD Breakout Board, ADIS16IMU/PCBZ The ADIS16IMU1/PCBZ (sold separately) provides a breakout board function for the ADIS16485, which means that it provides access to the ADIS16485 through larger connectors that support standard 1 mm ribbon cabling. It also provides four mounting holes for attachment of the ADIS16485 to the breakout board. For more information on the ADIS16IMU1/PCBZ, see https://www.analog.com/en/evaluation/eval-adis16imu1/eb.html. 1 CURRENT PC-Based Evaluation, EVAL-ADIS2 Use the EVAL-ADIS and the ADIS16IMU1/PCBZ to evaluate the ADIS16485 on a PC-based platform. CH1 2.00V CH4 100mA Ω POWER SUPPLY CONSIDERATIONS 10666-129 4 100ms/DIV Figure 29. Transient Current Demand, Start-Up The ADIS16485 has approximately ~24 µF of capacitance across the VDD and GND pins. While this capacitor bank provides a large amount of localized filtering, it also presents an opportunity for excessive charging current when the VDD voltage ramps too quickly. Use the following relationship to help determine the appropriate VDD voltage profile, with respect to any current limit functions that can cause the power supply to lose regulation and potentially introduce unsafe conditions for the ADIS16485. T CURRENT i(t ) = C dV dt 4 CH4 100mA Ω 1.00ms 1.00MS/s CH1 T 9.800% 1M POINTS 2.72V 10666-128 In addition to managing the initial voltage ramp, take note of the transient current demand that the ADIS16485 requires during its start-up/self-initialization process. Once VDD reaches 2.85 V, the ADIS16485 begins its start-up process. Figure 29 offers a broad connection that communicates when to expect the spikes in current, and Figure 30 provides more detail on the current/time behavior during the peak transient condition, which typically occurs approximately 350 ms after VDD reaches 2.85 V. In Figure 30 notice that the peak current approaches 600 mA and the transient condition lasts for approximately 1.75 ms. Figure 30. Transient Current Demand, Peak Demand X-RAY SENSITIVITY Exposure to high dose rate X-rays, such as those in production systems that inspect solder joints in electronic assemblies, may affect accelerometer bias errors. For optimal performance, avoid exposing the ADIS16485 to this type of inspection. Rev. H | Page 31 of 32 ADIS16485 Data Sheet OUTLINE DIMENSIONS 44.254 44.000 43.746 Ø 2.40 BSC (4 PLACES) 39.854 39.600 39.346 15.00 BSC 2.20 BSC 20.10 19.80 19.50 (8 PLACES) DETAIL A PIN 1 8.25 BSC 42.854 42.600 42.346 1.942 1.642 1.342 1.00 BSC 47.254 47.000 46.746 DETAIL A BOTTOM VIEW 14.254 14.000 13.746 DETAIL B FRONT VIEW 6.50 BSC 5.50 BSC 5.50 BSC 2.84 BSC 1.00 BSC PITCH DETAIL B 0.30 SQ BSC 12-07-2012-E 3.454 3.200 2.946 Figure 31. 24-Lead Module with Connector Interface [MODULE] (ML-24-6) Dimensions shown in millimeters ORDERING GUIDE Model1 ADIS16485BMLZ 1 Temperature Range −40°C to +105°C Package Description 24-Lead Module with Connector Interface [MODULE] Z = RoHS Compliant Part. ©2012−2019 Analog Devices, Inc. All rights reserved. Trademarks and registered trademarks are the property of their respective owners. D10666-0-2/19(H) Rev. H | Page 32 of 32 Package Option ML-24-6