What is Inertial Sensor

Inertial Sensor is a very important category in the Electrical & Electronics industry. A good Inertial Sensor can make a big difference in your comfort and productivity. There are many styles of Inertial Sensor available, so you can choose one that's well suited to your needs.

How to source & buy Inertial Sensor

At made-in-china.com, Inertial Sensor are made from various kinds of features such as Type, Servo, Capacitive, Piezoresistive, which offer unique user experiences to every kind of taste.
Take Type for example, you can find Servo Type, Capacitive Type and more.

By Type

The Best Inertial Sensor Products

IMU488M Hight Performance Inertial Navigation System (IMU) Inertial Measurement Unit Inertial Sensor Main Features - Precision 10 DoF MEMS Inertial Measurement Unit - Dynamic Range: Gyro &plusmn;450&deg;/s, Acc &plusmn;16g - Bias Stability: Gyro: 1&deg;/h, Acc 30&mu;g (Allan) - Full Temperature Range Accuracy Assured: Built-in High Performance Temperature Calibration and Compensation Algorithm - High Bandwidth, SPI Sampling Rate up to 2000Hz - Working Temperature: -40~+85&deg;C Brief Introduction IMU488M Inertial Measurement Unit is a high performance tactical grade MEMS Inertial Measurement Unit, which MEMS gyroscope enjoys 1&deg;/h (Allan) bias stability and MEMS accelerometer enjoys 30&mu;g (Allan) bias stability, and it can output precise 3-axis outputs of angular rate, 3 axis acceleration data, 3 axis magnetometer data, and barometer data, etc. IMU488M Inertial Measurement Unit adopts latest MEMS technology and advanced MEMS components, and IMU488M has been produced in bulk, which reduces the cost deeply. IMU488M enjoys excellent measurement performance, small size, light weight, and high reliability and robustness, it can output precise measurement data in harsh environment, and it has been widely applied in tactical unmanned aerial vehicles, intelligent driving, surface vehicle, platform stabilization, precise guided bomb, industrial robotics, etc. Technical Specifications Parameter Test Condition Value Unit Min Typical Max Gyroscopes Dynamic Range &plusmn;450 &deg;/s Bias Stability Allan variance 1 &deg;/h 10s average (-40~+85&deg;C, fixed temp.) Radom Walk 0.1 &ordm;/&radic;h Bias Repetition 4 &deg;/h Bais Bias change at full temp. range1 &plusmn;0.04 &deg;/s Bias change in vibration conditions2 6 &deg;/h Scale Factor Nonlinearity 100 ppm Resolution 3.052*10-7 &ordm;/s/LSB Bandwidth 200 Hz Accelerometer Dynamic Range &plusmn;16 g Bias Stability Allan variance 0.03 0.045 mg 10s average (-40~+85&deg;C, fixed temp.) 0.06 mg Radom Walk 0.01 m/s/&radic;h Bias Repetition 0.06 mg Scale factor nonlinearity 100 ppm Resolution 1.221*10-8 g/LSB Bandwidth 200 Hz Magnetometer Dynamic Range &plusmn;2 Gauss Resolution 120 uGauss Noise RMS 10Hz 50 uGauss Bandwidth 200 Hz Barometer Pressure Range 450 1100 mbar Resolution 0.1 mbar Absolute Accuracy 1.5 mbar Communication Interface 1 Channel SPI Baud rate 25 MHz 1 Channel UART Baud rate 230.4 Kbps Sampling Rate SPI 2000 Hz UART 200 Hz Electronic Characteristics Voltage 3 3.3 3.6 V Power Consumption 1.5 W Ripple Wave P-P 100 mV Physical Characteristics Dimension 47*44*14 mm Weight 50 grams Working Environment Working Temperature -40 85 &deg;C Storage Temperature -45 105 &deg;C Vibration Resistance 20~2000Hz, 6.06g Shock Resistance 1000g, 0.5ms Reliability MTBF 20000 h Continuous Working Time 120 h 1: The bias value is calculated based on the whole temperature change peroid, the temperature changing rate<=2&deg;C/minute, temperature range:-40~+85&deg;C; 2: (before vibration average value +after vibration average value) /2-during vibration average value, the vibration conditions are 6.06g, 20~2000Hz Typical Applications - Tactical Unmanned Aerial Vehicles - Intelligent Driving - Surface Vehicle - Platform Stabilization - Precise Guided Bomb - Industr

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