Datasheet ADIS16480 (Analog Devices) - 7

制造商Analog Devices
描述Ten Degrees of Freedom MEMS Inertial Sensor with Dynamic Orientation Outputs
页数 / 页45 / 7 — ADIS16480. Data Sheet. Parameter. Test Conditions/Comments. Min. Typ. …
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ADIS16480. Data Sheet. Parameter. Test Conditions/Comments. Min. Typ. Max. Unit

ADIS16480 Data Sheet Parameter Test Conditions/Comments Min Typ Max Unit

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ADIS16480 Data Sheet Parameter Test Conditions/Comments Min Typ Max Unit
POWER SUPPLY, VDD Operating voltage range 3.0 3.6 V Power Supply Current13 Normal mode, VDD = 3.3 V, µ ± σ 254 mA Sleep mode, VDD = 3.3 V 12.2 mA Power-down mode, VDD = 3.3 V 45 µA POWER SUPPLY, VDDRTC Operating voltage range 3.0 3.6 V Real-Time Clock Supply Current Normal mode, VDDRTC = 3.3 V 13 µA 1 Accuracy specifications assume calibration of accelerometers and magnetometers to address sensor drift and local influences on magnetic fields. 2 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. 3 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. 4 The relative error assumes that the initial error, at 25°C, is corrected in the end application. 5 Specification assumes a full scale (FS) of 1000 mbar. 6 The digital I/O signals use a 3.3 V system. 7 RST and CS pins are connected to the VDD pin through 10 kΩ pull-up resistors. 8 Endurance is qualified as per JEDEC Standard 22, Method A117, and measured at −40°C, +25°C, +85°C, and +125°C. 9 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. 10 These times do not include thermal settling, internal filter response times, or EKF start-up times (~825 ms), which may affect overall accuracy, with respect to time. 11 The RST line must be in a low state for at least 10 μs to assure a proper reset initiation and recovery. 12 The device functions at clock rates below 0.7 kHz, but at reduced performance levels. 13 Supply current transients can reach 600 mA during start-up and reset recovery. Rev. G | Page 6 of 44 Document Outline Features Applications General Description Functional Block Diagram Revision History Specifications Timing Specifications Timing Diagrams Absolute Maximum Ratings ESD Caution Pin Configuration and Function Descriptions Typical Performance Characteristics Basic Operation Register Structure SPI Communication Device Configuration Dual Memory Structure Reading Sensor Data User Registers Output Data Registers Inertial Sensor Data Format Rotation Rate (Gyroscope) Acceleration Delta Angles Delta Velocity Magnetometers Roll, Pitch, Yaw Angles Initial Conditions Quaternion Euler Angles Rotation Matrix Data Barometer Internal Temperature Status/Alarm Indicators Firmware Revision Product Identification Digital Signal Processing Gyroscopes/Accelerometers Averaging/Decimation Filter Magnetometer/Barometer FIR Filter Banks Filter Memory Organization Default Filter Performance Extended Kalman Filter Algorithm Covariance Terms Reference Frame Reference Transformation Matrix Declination Adaptive Operation Adaptive EKF Enable Bit Automatic EKF Divergence Reset Control Bit Gyroscope Fade Control Bit Body Frame/Local Navigation Frame Bit Orientation Format Control Bit Magnetometer Disable Control Bit Gravity Removal Control Bit Linear Acceleration/Magnetic Disturbance Detection Calibration Gyroscopes Manual Bias Correction Manual Sensitivity Correction Linear Acceleration on Effect on Gyroscope Bias Accelerometers Manual Bias Correction Manual Sensitivity Correction Magnetometers Hard Iron Correction Soft Iron Correction Matrix Barometers Restoring Factory Calibration Point of Percussion Alignment Alarms Static Alarm Use Dynamic Alarm Use Alarm Example System Controls Global Commands Software Reset Automatic Self-Test Memory Management Flash Memory Test General-Purpose I/O Data-Ready Indicator Input Sync/Clock Control General-Purpose I/O Control Power Management General-Purpose Registers Real-Time Clock Configuration/Data Applications Information Mounting Tips Evaluation Tools Breakout Board, ADIS16IMU1/PCB PC-Based Evaluation, EVAL-ADIS2 Power Supply Considerations Outline Dimensions Ordering Guide