Allicdata Part #: | ADXRS453BEYZ-ND |
Manufacturer Part#: |
ADXRS453BEYZ |
Price: | $ 0.00 |
Product Category: | Sensors, Transducers |
Manufacturer: | Analog Devices Inc. |
Short Description: | IC GYROSCOPE ANGULAR CLCC |
More Detail: | Gyroscope X (Pitch), Y (Roll) ±300 77.5Hz SPI 14-C... |
DataSheet: | ADXRS453BEYZ Datasheet/PDF |
Quantity: | 506 |
Series: | -- |
Packaging: | Tray |
Part Status: | Active |
Type: | Digital |
Axis: | X (Pitch), Y (Roll) |
Range °/s: | ±300 |
Sensitivity (LSB/(°/s)): | 80 |
Sensitivity (mV/°/s): | -- |
Bandwidth: | 77.5Hz |
Output Type: | SPI |
Voltage - Supply: | 3.15 V ~ 5.25 V |
Current - Supply: | 6mA |
Features: | Temperature Compensated |
Operating Temperature: | -40°C ~ 105°C (TA) |
Package / Case: | 14-CLCC |
Base Part Number: | ADXRS453 |
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Introduction to ADXRS453BEYZ
ADXRS453BEYZ is a three-axis high-precision, low-g gyroscope with integrated signal conditioning, temperature compensation, and amplitude compensation. It is part of the family of motion sensors and gyroscopes produced by Analog Devices. This gyroscope is unique in that it provides the user with high-resolution attitude measurements—the pitch, yaw, and roll of the object in which it is mounted—at an extremely low power requirement. This makes the ADXRS453BEYZ a great choice for applications that require minimal power consumption.
Application Field
The ADXRS453BEYZ is well-suited for applications such as high-precision unmanned aerial vehicles (UAVs), autonomous robotic systems, and various automated self-stabilization systems—especially those for which power utilization is a concern. It also excels in applications where fine-detailed measurements of small motions or orientation changes are required, such as in missile guidance systems, boom operation, and in-flight attitude control. In addition, its low-amplitude noise and low aging/zero bias make it ideal for mission-critical applications, such as medical and aerospace navigation and guidance systems.
Working Principle
The ADXRS453BEYZ utilizes a control loop and field-oriented drive to achieve its high-precision attitude measurements. This control loop operates on the differences between a measured lost rotation and a nominal reference amount. In addition, the field-oriented drive of the gyroscope further increases its precision. This is accomplished by comparing the angular rate signals with a reference gyroscope, and then adjusting their angle of stability in order to maintain commands more accurately.
Further, this gyroscope is able to provide high-precision output readings due to its onboard signal-processing circuit. This circuit integrates the angular rate signals that out of the sensing elements. These integrated signals are then passed to the gyroscope\'s onboard signal-processing circuit, where they are further optimized with proportional-integral controllers, and then used to calculate and output the pitch, yaw, and roll of the gyroscope\'s platform.
Conclusion
The ADXRS453BEYZ is an excellent choice for precision attitude measurement applications, due to its low power requirement, precision control loop, field-oriented drive, and onboard signal-processing circuit. Its low-amplitude noise, low aging/zero bias, and high-resolution make it suitable for many mission-critical situations, such as medical and aerospace navigation and guidance. With its unique features, the ADXRS453BEYZ can be a reliable and dependable addition to any system requiring high-precision gyroscopic measurements.
The specific data is subject to PDF, and the above content is for reference
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