Datasheet ADIS16497 (Analog Devices)
Hersteller | Analog Devices |
Beschreibung | Tactical Grade, Six Degrees of Freedom Inertial Sensor |
Seiten / Seite | 40 / 1 — Tactical Grade, Six Degrees of Freedom. Inertial Sensor. Data Sheet. … |
Revision | B |
Dateiformat / Größe | PDF / 1.2 Mb |
Dokumentensprache | Englisch |
Tactical Grade, Six Degrees of Freedom. Inertial Sensor. Data Sheet. ADIS16497. FEATURES. GENERAL DESCRIPTION
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Tactical Grade, Six Degrees of Freedom Inertial Sensor Data Sheet ADIS16497 FEATURES GENERAL DESCRIPTION Triaxial, digital gyroscope
The ADIS16497 is a complete inertial system that includes a
±125°/sec, ±450°/sec, ±2000°/sec range options
triaxis gyroscope and a triaxis accelerometer. Each inertial sensor
±0.05° axis to axis misalignment error
in the ADIS16497 combines industry leading iMEMS® technology
±0.25° (maximum) axis to package misalignment error
with signal conditioning that optimizes dynamic performance.
0.8°/hr in-run bias stability
The factory calibration characterizes each sensor for sensitivity,
0.09°/√hr angular random walk
bias, alignment, and linear acceleration (gyroscope bias). As a
Triaxial, digital accelerometer, ±40 g
result, each sensor has its own dynamic compensation formulas that
13 μg in run bias stability
provide accurate sensor measurements.
Triaxial, delta angle and delta velocity outputs
The ADIS16497 provides a simple, cost effective method for
Factory calibrated sensitivity, bias, and axial alignment
integrating accurate, multiaxis inertial sensing into industrial
Calibration temperature range: −40°C to +85°C
systems, especially when compared with the complexity and
SPI compatible
investment associated with discrete designs. All necessary motion
Programmable operation and control
testing and calibration are part of the production process at
Automatic and manual bias correction controls
the factory, greatly reducing system integration time. Tight
Configurable FIR filters
orthogonal alignment simplifies inertial frame alignment in
Digital I/O: data ready, external clock
navigation systems. The serial peripheral interface (SPI) and
Sample clock options: internal, external, or scaled
register structure provide a simple interface for data col ection
On demand self test of inertial sensors
and configuration control.
Single-supply operation: 3.0 V to 3.6 V 1500 g mechanical shock survivability
The footprint and connector system of the ADIS16497 enable a
Operating temperature range: −40°C to +105°C
simple upgrade from the ADIS16375, ADIS16480, ADIS16485, ADIS16488A, and ADIS16490. The ADIS16497 is available in an
APPLICATIONS
aluminum package that is approximately 47 mm × 44 mm ×
Precision instrumentation, stabilization
14 mm and includes a standard connector interface.
Guidance, navigation, control Avionics, unmanned vehicles Precision autonomous machines, robotics FUNCTIONAL BLOCK DIAGRAM DIO1 DIO2 DIO3 DIO4 RST VDD POWER SELF TEST I/O GND MANAGEMENT OUTPUT TRIAXIAL CS DATA GYROSCOPE REGISTERS SCLK CALIBRATION TRIAXIAL CONTROLLER SPI AND ACCELEROMETER FILTERS DIN USER TEMPERATURE CONTROL SENSOR REGISTERS DOUT CLOCK
001
ADIS16497
15061- Figure 1.
Rev. A 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 One Technology Way, P.O. Box 9106, Norwood, MA 02062-9106, U.S.A. license is granted by implication or otherwise under any patent or patent rights of Analog Devices. Tel: 781.329.4700 ©2017 Analog Devices, Inc. All rights reserved. Trademarks and registered trademarks are the property of their respective owners. Technical Support www.analog.com
Document Outline FEATURES APPLICATIONS GENERAL DESCRIPTION FUNCTIONAL BLOCK DIAGRAM TABLE OF CONTENTS REVISION HISTORY SPECIFICATIONS TIMING SPECIFICATIONS Register Specific Stall Times Timing Diagrams ABSOLUTE MAXIMUM RATINGS THERMAL RESISTANCE ESD CAUTION PIN CONFIGURATION AND FUNCTION DESCRIPTIONS TYPICAL PERFORMANCE CHARACTERISTICS THEORY OF OPERATION INERTIAL SENSOR SIGNAL CHAIN Gyroscope Data Sampling Accelerometer Data Sampling External Clock Options Inertial Sensor Calibration Gyroscope Factory Calibration Accelerometer Factory Calibration Filtering REGISTER STRUCTURE SERIAL PERIPHERAL INTERFACE DATA READY READING SENSOR DATA Burst Read Function DEVICE CONFIGURATION Dual Memory Structure USER REGISTER MEMORY MAP USER REGISTER DEFINTIONS PAGE NUMBER (PAGE_ID) DATA/SAMPLE COUNTER (DATA_CNT) STATUS/ERROR FLAG INDICATORS (SYS_E_FLAG) SELF TEST ERROR FLAGS (DIAG_STS) INTERNAL TEMPERATURE (TEMP_OUT) GYROSCOPE DATA Gyroscope Measurement Range/Scale Factor Gyroscope Data Formatting X-Axis Gyroscope (X_GYRO_LOW, X_GRYO_OUT) Y-Axis Gyroscope (Y_GYRO_LOW, Y_GYRO_OUT) Z-Axis Gyroscope (Z_GYRO_LOW, Z_GYRO_OUT) ACCELERATION DATA X-Axis Accelerometer (X_ACCL_LOW, X_ACCL_OUT) Y-Axis Accelerometer (Y_ACCL_LOW, Y_ACCL_OUT) Z-Axis Accelerometer (Z_ACCL_LOW, Z_ACCL_OUT) Accelerometer Resolution TIME STAMP CYCLICAL REDUNDANDCY CHECK (CRC-32) DELTA ANGLES Delta Angle Measurement Range X-Axis Delta Angle (X_DELTANG_LOW, X_DELTANG_OUT) Y-Axis Delta Angle (Y_DELTANG_LOW, Y_DELTANG_OUT) Z-Axis Delta Angle (Z_DELTANG_LOW, Z_DELTANG_OUT) Delta Angle Resolution DELTA VELOCITY X-Axis Delta Velocity (X_DELTVEL_LOW, X_DELTVEL_OUT) Y-Axis Delta Velocity (Y_DELTVEL_LOW, Y_DELTVEL_OUT) Z-Axis Delta Velocity (Z_DELTVEL_LOW, Z_DELTVEL_OUT) Delta Velocity Resolution Burst Read Command, BURST_CMD Product Identification, PROD_ID USER BIAS/SCALE ADJUSTMENT Gyroscope Scale Adjustment, X_GYRO_SCALE Gyroscope Scale Adjustment, Y_GYRO_SCALE Gyroscope Scale Adjustment, Z_GYRO_SCALE Accelerometer Scale Adjustment, X_ACCL_SCALE Accelerometer Scale Adjustment, Y_ACCL_SCALE Accelerometer Scale Adjustment, Z_ACCL_SCALE Gyroscope Bias Adjustment, XG_BIAS_LOW, XG_BIAS_HIGH Gyroscope Bias Adjustment, YG_BIAS_LOW, YG_BIAS_HIGH Gyroscope Bias Adjustment, ZG_BIAS_LOW, ZG_BIAS_HIGH Accelerometer Bias Adjustment, XA_BIAS_LOW, XA_BIAS_HIGH Accelerometer Bias Adjustment, YA_BIAS_LOW, YA_BIAS_HIGH Accelerometer Bias Adjustment, ZA_BIAS_LOW, ZA_BIAS_HIGH SCRATCH REGISTERS, USER_SCR_X FLASH MEMORY ENDURANCE COUNTER, FLSHCNT_LOW, FLSHCNT_HIGH GLOBAL COMMANDS, GLOB_CMD Software Reset Clear User Calibration Flash Memory Update On Demand Self Test (ODST) Bias Correction Update AUXILIARY I/O LINE CONFIGURATION, FNCTIO_CTRL Data Ready Indicator Input Sync/Clock Control GENERAL-PURPOSE I/O CONTROL, GPIO_CTRL MISCELLANEOUS CONFIGURATION, CONFIG Point of Percussion LINEAR ACCELERATION ON EFFECT ON GYROSCOPE BIAS DECIMATION FILTER, DEC_RATE CONTINUOUS BIAS ESTIMATION (CBE), NULL_CNFG SCALING THE INPUT CLOCK (PPS MODE), SYNC_SCALE Measurement Range Identifier, RANG_MDL FIR FILTERS FIR Filters Control, FILTR_BNK_0, FILTR_BNK_1 FIR Filter Bank Memory Maps FIR Filter Bank A, FIR_COEF_A000 to FIR_COEF_A119 FIR Filter Bank B, FIR_COEF_B000 to FIR_COEF_B119 FIR Filter Bank C, FIR_COEF_C000 to FIR_COEF_C119 FIR Filter Bank D, FIR_COEF_D000 to FIR_COEF_D119 Default Filter Performance FIRMWARE REVISION, FIRM_REV FIRMWARE REVISION YEAR, FIRM_Y BOOT REVISION NUMBER, BOOT_REV CONTINUOUS SRAM TESTING Signature CRC, Calibration Values, CAL_SIGTR_LWR Signature CRC, Calibration Values, CAL_SIGTR_UPR Derived CRC, Calibration Values, CAL_DRVTN_LWR Derived CRC, Calibration Values, CAL_DRVTN_UPR Signature CRC, Program Code, CODE_SIGTR_LWR Signature CRC, Program Code, CODE_SIGTR_UPR Derived CRC, Program Code, CODE_DRVTN_LWR Derived CRC, Program Code, CODE_DRVTN_UPR Lot Specific Serial Number, SERIAL_NUM APPLICATIONS INFORMATION MOUNTING BEST PRACTICES PREVENTING MISINSERTION EVALUATION TOOLS Breakout Board, ADIS16IMU1/PCBZ PC-Based Evaluation, EVAL-ADIS2 POWER SUPPLY CONSIDERATIONS OUTLINE DIMENSIONS ORDERING GUIDE