IMU Accelerometer Gyro

Stim300 MEMS Inertial Measurement Unit with RS-422 Serial Interface The MEMS inertial measurement unit integrates a three-axis gyroscope, three-axis accelerometer, three-axis inclination angle sensor, temperature sensor, signal processing board, and necessary software. It precisely measures three-axis angular rate, three-axis acceleration, and three-axis inclination angle of a carrier, outputting compensated data (including temperature, installation misalignment, and

Stim300 IMU Drone Flight Controller with 0.1°/h Gyro Stability The MEMS inertial measurement unit consists of a three-axis gyroscope, three-axis accelerometer, three-axis inclination angle sensor, temperature sensor, signal processing board, and necessary software. It measures three-axis angular rate, three-axis acceleration, and three-axis inclination angle of a carrier, outputting compensated data (including temperature, installation misalignment, and nonlinear compensation

Three-Axis Gyro Accelerometer Integrated Inertial Measurement Unit with RS422 Output Key Specifications Gyro Measuring range: ±400°/s In-Run Bias Stability: 0.3°/h Angular Random Walk: 0.15º/√h Bias repeatability (1σ): 1°/h Scale Factor Non-Linearity (1σ): 150ppm 3 dB Bandwidth: 250Hz Accelerometer bias stability: 0.02mg Weight: 55g Product Overview The IMU6 MEMS Inertial Measurement Unit is a high-performance sensor module integrating: Three-axis gyroscope Three-axis

Strong Shock Vibration Inertial Measurement Unit Sensor for Aerospace Defense RS-422 Output Key Specifications Attribute Value Gyro Measuring range ±400°/s Bias Stability 0.3°/h Angular Random Walk 0.15º/√h Bias repeatability (1σ) 1°/h Scale Factor Repeatability (1σ) 150ppm 3 dB Bandwidth 250Hz Accelerometer bias stability 0.02mg Weight 55g Misalignment ±0.05° Power consumption 2W Product Overview The IMU6 MEMS Inertial Measurement Unit is a highly integrated sensing system

Tactical Grade Inertial Measurement Unit without GPS aided Stim300 Replacement Key Specifications Attribute Value Gyro Measuring range ±400°/s In-Run Bias Stability 0.3°/h Angular Random Walk 0.15º/√h Bias repeatability (1σ) 1°/h Scale Factor Non-Linearity(1σ) 150ppm 3 dB Bandwidth 250Hz Accelerometer bias stability 0.02mg Weight 55g Product Overview The IMU6 MEMS inertial measurement unit integrates a three-axis gyroscope, three-axis accelerometer, three-axis inclination

High Performance MEMS Inertial Measurement Unit with Built-in 3 Axis Accelerometer and Gyroscope The MEMS inertial measurement unit consists of three-axis gyroscope, three-axis accelerometer, three-axis inclination angle sensor, temperature sensor, signal processing board, structure and necessary software. It measures the three-axis angular rate, three-axis acceleration and three-axis inclination angle of a carrier, and outputs the gyro, accelerometer and inclination data

Low Drift Inertial Measurement Unit with Built-in 3 Axis Accelerometer and Gyroscope The IMU6 inertial measurement unit integrates a three-axis gyroscope, three-axis accelerometer, temperature sensor, and signal processing board to measure angular rate, acceleration, and tilt angle of the carrier. The system outputs compensated data (including temperature compensation, installation misalignment angle compensation, and nonlinear compensation) through an RS-422 serial port

Industrial Grade IMU Inertial Measurement Unit Sensor STIM300 Replacement Low Noise Key Specifications Attribute Value Gyro Range ±400°/s Gyro zero bias stability ≤0.5°/h Acc Range 30g Scale factor nonlinearity 0.02mg Power Supply 5V Bandwidth 125Hz Product Overview The MEMS inertial measurement unit integrates a three-axis gyroscope, three-axis accelerometer, three-axis inclinometer, temperature sensor, signal processing board, and supporting software. This comprehensive

Light Weight MEMS IMU Inertial Measurement Unit 400°/s for Industry Key Specifications Attribute Value Gyro Range ±400°/s Gyro Zero Bias Stability 0.5°/h Acc Range ±30g Acc Zero Bias Stability 0.05mg Bandwidth 125 Hz Random walk 0.1°/√h Interface RS-422 Power Supply 5V Product Description The MEMS inertial measurement unit consists of: Three-axis gyroscope Three-axis accelerometer Three-axis inclination angle sensor Temperature sensor Signal processing board Structural

16488HB 10-Axis MEMS Inertial Measurement Unit | ADIS16488 Drop-In Replacement IMU Sensor Product Description The 16488HB multi-degree-of-freedom MEMS inertial measurement unit IMU sensor is a complete 10-axis inertial navigation system INS integrating a triaxial MEMS gyroscope angular rate sensor, a triaxial digital accelerometer, a triaxial magnetometer electronic compass, and a high-precision barometric pressure sensor altimeter. Engineered as a pin-compatible ADIS16488

RS422 Output IMU Six Output Inertial Sensor Analog Of STIM300 Electrical Interface The electrical connector of IMU300C-A0-IMU product is J30J-15 TJL, with the following contact definition: Stitch number Name Type Remark 1 TxD- Output RS422 2 RxD- Input RS422 3 TST_1 Output 4 TOV_1 Output 5 RST Input 6 GND Input 7 Spare 8 VCC_5V Power source +5v 9 TxD+ Output RS422 10 RxD+ Input RS422 11 ExtTrig Input Synchronous input 5V 12 GND Input 13 GND Input 14 Spare 15 GND Power ground

6-Axis IMU with 3-Axis Accelerometer Gyroscope Stim300 Replacement Product Feature This MEMS inertial measurement unit integrates: Three-axis gyroscope Three-axis accelerometer Three-axis inclination angle sensor Temperature sensor Signal processing board The unit measures three-axis angular rate, acceleration, and inclination angle of a carrier. It outputs compensated gyro, accelerometer, and inclination data through an RS-422 serial port using a defined communication

High-performance FOG IMU with 0.8°/h bias stability, 200Hz bandwidth, and 200g accelerometer range. Compact 47×44×14mm design withstands extreme environments (-40°C to +80°C) and strong vibration. Ideal for UAVs, surveying, and stabilization platforms.

High-precision 9DOF IMU with 0.8°/h gyro bias stability, 200g accelerometer range, and 200Hz bandwidth. Certified for -40℃ to +80℃ operation, 20,000h MTBF reliability, and withstands 1000G impact. Ideal for gimbal stabilization and unmanned systems.

ADIS16495 tactical grade IMU delivers 0.8°/h gyro bias stability & 0.06mg accelerometer stability. With 200Hz bandwidth, 2000°/s range, and robust construction (6.06G vibration, 1000G impact resistance), it ensures precision for unmanned systems & industrial stabilization.

Compact 16488HB MEMS IMU for UAVs: ±2000°/s gyro, ±200g accelerometer, 0.8°/h bias stability. Withstands 1000g impact, -40°C to +80°C operation, 20,000h MTBF. Ideal for harsh industrial environments.

Product Overview Engineered with advanced MEMS technology, the 16488HB IMU delivers accurate 3-axis angular velocity and 3-axis acceleration data for industrial and commercial applications. Equipped with a triaxial magnetometer (2.5gauss) and digital barometer (300-1100mbar), it supports high-precision positioning and motion tracking. Designed to withstand 1000G impact and 6.06G vibration, it excels in unmanned motion carriers, communication in motion, and mapping projects.

1. Product Overview The 16488HB is an inertial measurement unit (IMU) based on micro-mechanical technology (MEMS), with built-in high-performance MEMS gyroscope and MEMS accelerometer, outputting 3 angular velocities and 3 accelerations. The 16488HB has high reliability and strong environmental adaptability. By matching different software, the product can be widely used in unmanned motion carrier, mobile communication, mapping and other fields. 2. Product Features 1) Three

High Stability Fiber Optic Angular Rate Sensor for Surveying & North Seeking The MFOG-24 micro-nano fiber optic gyroscope is a high-precision angular rate sensor integrating optical, mechanical, and electronic technologies . Based on the Sagnac effect , it incorporates a variety of micro-nano fiber optic devices and realizes angular rate detection by measuring, processing, and feedback-controlling the phase difference generated by two counter-propagating light beams. The

10-Axis IMU Sensor with ±0.8°/h Bias Stability High-performance inertial measurement unit designed for drone attitude control applications requiring exceptional precision and low noise characteristics. Product Overview The 16488HB Inertial Measurement Unit delivers exceptional performance with its three-axis gyroscope and accelerometer. Engineered for precision applications, this unit provides enhanced stability and reliability, making it an ideal replacement for the Adis