Datasheet ADXC1501 (Analog Devices)
Fabricante | Analog Devices |
Descripción | Combined Gyroscope and Tri-Axis Accelerometer |
Páginas / Página | 2 / 1 — Combined Gyroscope. and 3-Axis Accelerometer. Data Sheet. ADXC1501. … |
Revisión | Sp0 |
Formato / tamaño de archivo | PDF / 87 Kb |
Idioma del documento | Inglés |
Combined Gyroscope. and 3-Axis Accelerometer. Data Sheet. ADXC1501. FEATURES. GENERAL DESCRIPTION
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Combined Gyroscope and 3-Axis Accelerometer Data Sheet ADXC1501 FEATURES GENERAL DESCRIPTION Combined gyroscope and 3-axis, low g accelerometer
The ADXC1501 is a yaw rate gyroscope and 3-axis accelerometer
Temperature compensated, high precision bias, and
combined in a single package. It is designed for electronic
sensitivity performance
stability control and other high performance applications that
±30 mg accelerometer bias stability over temperature
require yaw rate and acceleration signals simultaneously. An
±2°/sec gyroscope null stability over temperature
internal temperature sensor compensates offset and sensitivity
2.5 mg rms typical accelerometer noise at 35.6 Hz
performance, providing excellent stability over the −40°C to
0.1°/sec rms typical gyroscope noise at 35.6 Hz
+105°C temperature range.
Gyroscope: linear acceleration rejection of 0.03°/sec/g
A digital serial port interface (SPI) transmits the yaw rate and
Acceleration: ±32 g overload performance
acceleration data to a host microcontroller. A 4-bit cyclical
SPI digital output with a 16-bit data-word and a 4-bit CRC
redundancy check (CRC) provides fault coverage for the
Comprehensive electromechanical fail-safe features
transmitted SPI data, and internal fault detection routines
6 kHz data update rate
ensure the integrity of all reported yaw rates and acceleration
Programmable filter response
data. A fully integrated electromechanical continuous self test
<16 mA quiescent current draw
(CST) routine provides run-time diagnostic capability for
3.3 V or 5 V operation
assessing the health of each MEMS element.
−40°C to +105°C temperature range 16-lead SOIC package for robust EMI performance
An advanced gyroscope sensor design rejects the linear
Qualified for automotive applications
acceleration effects of shock and vibration, enabling the ADXC1501 to operate in harsh environments. The accelerometer signal
APPLICATIONS
chain is designed to prevent overload conditions from
Electronic stability control
occurring in these same harsh environments.
Chassis control
The ADXC1501 is designed to operate at either 3.3 V or 5 V. At less than 16 mA current consumption, the ADXC1501 can be used in energy sensitive applications.
FUNCTIONAL BLOCK DIAGRAM MISO MOSI SCLK CS SYNC TPA TPB ACCELERATION GYROSCOPE SENSOR SENSOR SPI INTERFACE REGISTERS/MEMORY TEST/DEBUG DIE DIE ADXC1501 Σ-∆ NVM MOD XY AFE CORIOLIS BAND- Σ-∆ Σ-∆ AFE PASS MOD FILTER MOD XY SENSOR ALU RESONATOR PHASE- CLOCK LOCKED Σ-∆ TEMP Z-AXIS AFE GENERATION LOOP MOD SENSOR GYROSCOPE TRIM SYSTEM AND CONTROLLER Σ-∆ Z SELF TEST MOD AFE Z SENSOR HIGH VOLTAGE GENERATION VOLTAGE REGULATION
01 0 9-
CP VSA VSD AVDD DVDD AGND DGND VSIO VCM
308 1 Figure 1. For more information about the ADXC1501, contact the Analog Devices, Inc., Customer Interaction Center at http://www.analog.com/technical_support to connect with a technical support specialist.
Rev. Sp0 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 NOTES