High Performance, Digital Output Gyroscope Features: Complete rate gyroscope on a single chip ±300°/sec angular rate sensing Ultrahigh vibration rejection: 0.01°/sec/g Excellent 16°/hour null bias stability Internal temperature compensation 2000 g powered shock survivability SPI Digital output with 16-bit data word Low noise and low power 3.3 V to 5 V operation -40°C to + 105°C operation Ultra small, light, and RoHS compliant Two package options: -- Low cost SOIC_CAV package for yaw rate (z-axis) response -- Innovative ceramic vertical mount package (LCC_V), which can be oriented for pitch, roll, or yaw response

Small, Low Power, 3-Axis 3 g Accelerometer

Accelerometers Small, Low Power, 3-Axis 3 g Accelerometer

Tri-Axis Analog Accel 10g/ 40g

Tri-Axis Digital Accel 10g/ 20g/ 40g

The ADIS16477 is a precision, miniature MEMS inertial measurement unit (IMU) that includes a triaxial gyroscope and a triaxial accelerometer. Each inertial sensor in the ADIS16477 combines with signal conditioning that optimizes dynamic performance. The factory calibration characterizes each sensor for sensitivity, bias, alignment, linear acceleration (gyroscope bias), and point of percussion (accelerometer location). As a result, each sensor has dynamic compensation formulas that provide accurate sensor measurements over a broad set of conditions.The ADIS16477 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, greatly reducing 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.The ADIS16477 is available in a 44-ball, ball grid array (BGA) package that is approximately 11 mm ? 15 mm ? 11 mm.Applications Navigation, stabilization, and instrumentation Unmanned and autonomous vehicles Smart agriculture/construction machinery Factory/industrial automation, robotics Virtual/augmented reality Internet of Moving Things

The ADXRS624 is a complete angular rate sensor (gyroscope) that uses the Analog Devices, Inc., surface-micromachining process to create a functionally complete and low cost angular rate sensor integrated with all required electronics on one chip. The manufacturing technique for this device is the same high volume BiMOS process used for high reliability automotive airbag accelerometers.The ADXRS624 is an automotive grade gyroscope. Automotive grade gyroscopes have more extensive guaranteed min/max specifications due to automotive testing.The output signal, RATEOUT (1B, 2A), is a voltage proportional to angular rate about the axis normal to the top surface of the package. The output is ratiometric with respect to a provided reference supply. A single external resistor between SUMJ and RATEOUT can be used to lower the scale factor. An external capacitor sets the bandwidth. Other external capacitors are required for operation. A temperature output is provided for compensation techniques. Two digital self-test inputs electromechanically excite the sensor to test proper operation of both the sensor and the signal conditioning circuits. The ADXRS624 is available in a 7 mm ? 7 mm ? 3 mm BGA chip scale package.APPLICATIONS Navigation systems Inertial measurement units Platform stabilization Robotics

ADXL362 MEDICAL IMPLANTABLE / REEL7

Mems Accelerometer, Analogue, X/Y/Z Axis Rohs Compliant: Yes |Analog Devices ADXL358CCCZ-RL7

MEMS ACCELEROMETER, 2G/4G/8G/16G, LGA14; MEMS Sensor Output: Digital; Measurement Axis: X, Y, Z; Acceleration Range: ± 2g, ± 4g, ± 8g, ± 16g; Supply Voltage Min: 2V; Supply Voltage Max: 3.6V; Sensor Case Style: LGA; No. of Pins: 14Pins; Sensitivity Typ: -; Sensitivity Min: -; Sensitivity Max: -; Product Range: -; Automotive Qualification Standard: -; MSL: MSL 3 - 168 hours; SVHC: No SVHC (07-Jul-2017)