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ADIS16IMU1/PCBZ Datasheet(PDF) 1 Page - Analog Devices

Part # ADIS16IMU1/PCBZ
Description  Six Degrees of Freedom Inertial Sensor
PDF  38 Pages
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Manufacturer  AD [Analog Devices]
Direct Link  http://www.analog.com
Logo AD - Analog Devices

ADIS16IMU1/PCBZ Datasheet(HTML) 1 Page - Analog Devices

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Six Degrees of Freedom Inertial Sensor
Data Sheet
ADIS16486
Rev. 0
Document Feedback
Information furnished by Analog Devices is believed to be accurate and reliable. However, no
responsibilityisassumedbyAnalogDevicesforitsuse,norforanyinfringementsofpatentsorother
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.Trademarksandregisteredtrademarksarethepropertyoftheirrespectiveowners.
One Technology Way, P.O. Box 9106, Norwood, MA 02062-9106, U.S.A.
Tel: 781.329.4700
©2020 Analog Devices, Inc. All rights reserved.
Technical Support
www.analog.com
FEATURES
Triaxial digital gyroscope, ±450°/sec dynamic range
(minimum)
±0.018° axis to axis misalignment error (typical)
5.3°/hr in-run bias stability (typical)
0.25°/√hr angular random walk (typical)
0.01% FS nonlinearity
Triaxial digital accelerometer, ±18 g dynamic range
(minimum)
Triaxial, delta angle, and delta velocity outputs
Factory calibrated sensitivity, bias, and axial alignment
Calibration temperature range: −40°C to +85°C
SPI compatible
Programmable operation and control
Automatic and manual bias correction controls
4 FIR filter banks, 120 configurable taps
Digital input and output: data ready alarm indicator,
external clock
Alarms for condition monitoring
Power-down and sleep mode for power management
Optional external sync input clock: 2.4 kHz (maximum)
Continuous self test of inertial sensors
On demand self test of inertial sensors
Continuous CRC-based memory testing
Single VDD power supply operation: 3.0 V to 3.6 V
2000 g mechanical shock survivability
Operating temperature range: −40°C to +105°C
APPLICATIONS
Attitude and heading reference systems
Platform stabilization and control
Unmanned vehicle navigation
Robotics and instrumentation
GENERAL DESCRIPTION
The ADIS16486 is a complete inertial system that includes a triaxis
gyroscope and a triaxis accelerometer. Each inertial sensor in the
ADIS16486 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). Therefore,
each sensor has dynamic compensation formulas that provide
accurate sensor measurements.
The ADIS16486 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, which reduces system integration time. Tight orthogonal
alignment simplifies inertial frame alignment in navigation
systems. The serial peripheral interface (SPI) and register structure
provide a simple interface for data collection and configuration
control. Parylene coating of all internal circuitry provides a
protective barrier against moisture exposure.
The ADIS16486 uses the same footprint and connector system as
the ADIS16480, ADIS16485, ADIS16487, and ADIS16488A, which
greatly simplifies the upgrade process. The ADIS16486 is packaged
in a module that is approximately 47 mm × 44 mm × 14 mm with
a 24-lead standard connector interface.
FUNCTIONAL BLOCK DIAGRAM
CONTROLLER
CLOCK
TRIAXIAL
GYROSCOPE
TRIAXIAL
ACCELEROMETER
POWER
MANAGEMENT
CS
SCLK
DIN
DOUT
GND
VDD
TEMPERATURE
VDD
DIO1 DIO2 DIO3 DIO4
VDDRTC
RST
SPI
SELF TEST
I/O
ALARMS
OUTPUT
DATA
REGISTERS
USER
CONTROL
REGISTERS
CALIBRATION
AND
FILTERS
ADIS16486
Figure 1.


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