Datasheet ADIS16467 (Analog Devices)

ManufacturerAnalog Devices
DescriptionPrecision MEMS IMU Module
Pages / Page34 / 1 — Precision, Miniature MEMs IMU. Preliminary Technical Data. ADIS16467. …
RevisionB
File Format / SizePDF / 600 Kb
Document LanguageEnglish

Precision, Miniature MEMs IMU. Preliminary Technical Data. ADIS16467. FEATURES. GENERAL DESCRIPTION. Triaxial, digital gyroscope

Datasheet ADIS16467 Analog Devices, Revision: B

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Precision, Miniature MEMs IMU Preliminary Technical Data ADIS16467 FEATURES GENERAL DESCRIPTION Triaxial, digital gyroscope
The ADIS16467 is a precision, miniature MEMS inertial measure-
±125°/sec, ±500°/sec, ±2000°/sec range models
ment unit (IMU) that includes a triaxial gyroscope and a triaxial
2°/hr in-run bias stability (ADIS16467-1)
accelerometer. Each inertial sensor in the ADIS16467 combines
0.15°/√hr angle random walk (ADIS16467-1 and
with signal conditioning that optimizes dynamic performance.
(ADIS16467-2)
The factory calibration characterizes each sensor for sensitivity,
±0.05° axis-to-axis misalignment error
bias, alignment, linear acceleration (gyroscope bias), and point
Triaxial, digital accelerometer, ±40 g
of percussion (accelerometer location). As a result, each sensor
13 μg in-run bias stability
has dynamic compensation formulas that provide accurate
Triaxial, delta angle and delta velocity outputs
sensor measurements over a broad set of conditions.
Factory calibrated sensitivity, bias, and axial alignment
The ADIS16467 provides a simple, cost effective method for
Calibration temperature range: −40°C to +85°C
integrating accurate, multiaxis inertial sensing into industrial
SPI compatible data communications
systems, especially when compared with the complexity and
Programmable operation and control
investment associated with discrete designs. All necessary motion
Automatic and manual bias correction controls
testing and calibration are part of the production process at the
Data ready indicator for synchronous data acquisition
factory, greatly reducing system integration time. Tight orthogonal
External sync modes: direct, pulse, scaled, and output
alignment simplifies inertial frame alignment in navigation
On demand self test of inertial sensors
systems. The serial peripheral interface (SPI) and register
On demand self test of flash memory
structure provide a simple interface for data collection and
Single-supply operation (VDD): 3.0 V to 3.6 V
configuration control.
2000 g mechanical shock survivability Operating temperature range: −40°C to +105°C
The ADIS16467 is in an aluminum module package that is approximately 22.4 mm × 24.3 mm × 9 mm and has a 14-pin
APPLICATIONS
connector interface.
Navigation, stabilization, and instrumentation Unmanned and autonomous vehicles Smart agriculture/construction machinery Factory/industrial automation, robotics Virtual/augmented reality Internet of Moving Things FUNCTIONAL BLOCK DIAGRAM DR RST VDD POWER SELF TEST I/O GND MANAGEMENT TRIAXIAL OUTPUT CS GYRO DATA REGISTERS SCLK TRIAXIAL CALIBRATION CONTROLLER SPI ACCEL AND FILTERS DIN USER TEMP CONTROL REGISTERS DOUT CLOCK ADIS16467
1 00
SYNC
439- 15 Figure 1.
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