Inertial Reference Unit

142 results for Inertial Reference Unit

Digital Output · Non-Customized · IP65

High Performance 6 Dof Inertial Measurement Unit

1 Piece  (MOQ)
IMU588M Hight Performance Tactical Inertial Measurement Unit Main Features - Precision 6 DoF MEMS Inertial Measurement Unit - Dynamic Range: Gyro ±450°/s, Acc ±16g (Z axis ±50g ) - Bias Stability: Gyro: 1°/h, Acc 30µg (Allan, ±16g) - Full Tempera

Piezoelectric · Customized · Digital Output

Imu Inertial Measurement Unit Imu16488 - Adis16488bmlz Inertial Measurement Unit Mems Imu

US$ 550-1100 / Piece
10 Pieces  (MOQ)
Product Description Inertial Measurement Unit (IMU) Our IMU is a cost-effective high performance Attitude and Heading Reference System (AHRS). It contains the best in class magnetic calibration procedure for optimal heading, and It is suitable for low to medium dynamic applications. Factory c

Piezoelectric · Customized · Digital Output

Tatical Grade Imu Inertial Measurement Unit Imu16488 - Adis16488bmlz Inertial Measurement Unit Mems Imu

US$ 550-1100 / Piece
10 Pieces  (MOQ)
Product Description Inertial Measurement Unit (IMU) Our IMU is a cost-effective high performance Attitude and Heading Reference System (AHRS). It contains the best in class magnetic calibration procedure for optimal heading, and It is suitable for low to medium dynamic applications. Factory c

Piezoelectric · Customized · Digital Output

China High Precision Low Weight Autonomous Navigation Inertial Measurement Unit (IMU) Syetem

US$ 550-1100 / Piece
10 Pieces  (MOQ)
Product Description Inertial Measurement Unit (IMU) Our IMU is a cost-effective high performance Attitude and Heading Reference System (AHRS). It contains the best in class magnetic calibration procedure for optimal heading, and It is suitable for low to medium dynamic applications. Fact

Digital Output · Customized · Three

High-Precision Aircraft Navigation Inertial Reference Navigation System with Ring Laser Gyroscobe Inertial Measurement Unit Imu

US$ 95800-104500 / Piece
1 Piece  (MOQ)
BELGA50B IMU for UAV: High-Performance Airborne Ring Laser Gyroscope INS System for Precise Navigation This high-performance Aircraft Inertial Navigation System (AINS) integrates a laser gyroscope and quartz accelerometer for ultra-stable motion sensing. Featuring strapdown architecture and AH

Digital Output · Non-Customized · IP67

Small Size Inertial Reference System

1 Piece  (MOQ)
IMU488M Hight Performance Inertial Measurement Unit Main Features - Precision 10 DoF MEMS Inertial Measurement Unit - Dynamic Range: Gyro ±450°/s, Acc ±16g - Bias Stability: Gyro: 1°/h, Acc 30μg (Allan) - Full Temperature Range Accuracy Assured: Built-in High Pe

Digital Output · Customized · Three

Advanced Inertial Navigation System with Ring Laser Gyroscope Rlg Inertial Sensor Imu for Uavs Inertial Reference

US$ 95800-104500 / Piece
1 Piece  (MOQ)
BELGA50B IMU for UAV: Compact Inertial Reference Unit (IRU) with Laser IMU for UAV Navigation This high-precision Aircraft Inertial Navigation System (AINS) features a laser gyroscope and quartz accelerometer. Utilizing advanced strapdown and modulation technology, it offers real-time, full-pa

Digital Output · Non-Customized · IP67

Inertial Reference System Used in Unmanned Aircraft

1 Piece  (MOQ)
IMU488M Hight Performance Inertial Measurement Unit Main Features - Precision 10 DoF MEMS Inertial Measurement Unit - Dynamic Range: Gyro ±450°/s, Acc ±16g - Bias Stability: Gyro: 1°/h, Acc 30μg (Allan) - Full Temperature Range Accuracy Assured: Built-in High Pe

Digital Output · Customized · Three

Cutting-Edge Aerospace Aircraft Navigation Inertial Reference Navigation System with Ring Laser Gyroscope Imu

US$ 125800-137300 / Piece
1 Piece  (MOQ)
BELGA50C Cutting-Edge Aerospace Aircraft Navigation Inertial Reference Navigation System with Integrated Ring Laser Gyroscope This aerospace inertial navigation system integrates a laser gyro and quartz accelerometer for high-precision navigation. Suitable for UAVs and special air vehicles, it

Digital Output · Non-Customized · IP67

Tactical Grade Inertial Reference System

1 Piece  (MOQ)
IMU488M Hight Performance Inertial Measurement Unit Main Features - Precision 10 DoF MEMS Inertial Measurement Unit - Dynamic Range: Gyro ±450°/s, Acc ±16g - Bias Stability: Gyro: 1°/h, Acc 30μg (Allan) - Full Temperature Range Accuracy Assured: Built-in High Pe
  • QWhat is an Inertial Reference Unit and how does it work in electronics applications?

    An Inertial Reference Unit is a device that measures and detects acceleration, rotation, and tilt. In electronics, it provides critical data for navigation, motion tracking, and stabilization. Partnering with a reputable manufacturer allows you access to the latest technologies and accurate sensing capabilities.

  • QHow can I verify the quality and certification of Inertial Reference Unit suppliers in China?

    To ensure quality and certification of Inertial Reference Unit suppliers in China, you can request documentation, such as ISO certificates or product testing reports. It is advisable to visit the supplier's manufacturing facilities or request samples for validation.

  • QWhat are the benefits of sourcing Inertial Reference Units in bulk for electronic applications?

    Purchasing Inertial Reference Units in bulk for electronic applications allows for cost savings, economies of scale, and ensures product availability for your ongoing projects. Bulk orders provide opportunities for customization, packaging options, and prompt delivery, allowing you to meet your electronic design requirements efficiently.

Honeywell TARS-HCASS Transportation Attitude Reference System Ruggedized Inertial Measurement Unit (IMU) TARS Series

US$ 130-599 / Piece
1 Piece  (MOQ)
The Transportation Attitude Reference System (TARS-IMU) is a packaged sensor array designed to report vehicle angular rate, acceleration, and attitude data for demanding applications in industries such as heavy-duty, off-highway transportation. The TARS-IMU enables autonomous vehicle characteris

Piezoelectric · Digital Output · IP67

2 Degree Bias Stability Gyroscope Integrated Inertial Navigation Sensor System Vertical Reference Unit Device

US$ 469-583 / Piece
1 Piece  (MOQ)
Main parameter Indication Unit Attitude angles Pitch/Roll angle 0.3 ° RMS Attitude ranges Roll Pitch ±180 ±90 ° RMS ° RMS Gyroscope Measurement range (can be customized) ±100 °/s Angle random walk 0.12 °/√h Linear scale fact

Digital Output · Customized · Three

Inertial Reference System with Ring Laser Gyroscope Rlg Inertial Measurement Unit Imu for Aerospace Inertial Navigation Applications

US$ 64200-70100 / Piece
1 Piece  (MOQ)
BELGA50A Inertial Reference System with RLG Gyro for Aerospace Applications This laser gyro inertial navigation system employs high-precision laser gyroscopes and quartz accelerometers, making it ideal for fixed-wing and rotary-wing UAVs. It supports multi-source information fusion, providing rea

Digital Output · Non-Customized · IP67

Inertial Reference System and Inertial Navigation System

1 Piece  (MOQ)
IMU488M Hight Performance Inertial Measurement Unit Main Features - Precision 10 DoF MEMS Inertial Measurement Unit - Dynamic Range: Gyro ±450°/s, Acc ±16g - Bias Stability: Gyro: 1°/h, Acc 30μg (Allan) - Full Temperature Range Accuracy Assured: Built-in High Pe

Piezoelectric · Digital Output · IP67

Low Price High Accuaracy Elliptical Altitude Heading Reference System Sensor Ahrs Uav Ugv Application

US$ 468-583 / Piece
1 Piece  (MOQ)
Main Parameters of the Device Attitude Angle -Heading angle -Roll/Pitch angle 0.2° RMS 0.2° RMS Angle Range -Pitch -Roll ±180°RMS ±90°RMS Gyroscope Range (Customized) &plusm

Piezoelectric · Digital Output · IP67

Vertical Reference Unit Module Measure The Angular Velocity and Acceleration Providing Non Reference Standard Heading Angles

US$ 469-583 / Piece
1 Piece  (MOQ)
Main parameter Indication Unit Attitude angles Pitch/Roll angle 0.3 ° RMS Attitude ranges Roll Pitch ±180 ±90 ° RMS ° RMS Gyroscope Measurement range (can be customized) ±100 °/s Angle random walk 0.12 °/√h Linear scale fact

Piezoelectric · Customized · Digital Output

Attitude Heading Reference System

US$ 550-1100 / Piece
10 Pieces  (MOQ)
Product Description Inertial Measurement Unit (IMU) Our IMU is a cost-effective high performance Attitude and Heading Reference System (AHRS). It contains the best in class magnetic calibration procedure for optimal heading, and It is suitable for low to medium dynamic applications. Factory c

Piezoresistive · ISO · Double

Dual-Axis High Precision Turntable for Inertial Navigation System Test Calibration

1 Piece  (MOQ)
Technical parameter Index name Indicator parameters Table structure O-O Structure Table structure Frame type Rated load weight 50kg Table weight ≤250kg Angular position Positioning accuracy ±36" (biaxial) Angular position repeated positioning accuracy &pl

Piezoelectric · Customized · Digital Output

Imu910 GPS/Insmems Combined Inertial Navigation System (IMU) Inertial Measuring Unit

US$ 550-1100 / Piece
10 Pieces  (MOQ)
Product Description Inertial Measurement Unit (IMU) Our IMU is a cost-effective high performance Attitude and Heading Reference System (AHRS). It contains the best in class magnetic calibration procedure for optimal heading, and It is suitable for low to medium dynamic applications. Factory c

Capacitive · Non-Customized · Analog Output

Very Low Noise Seismic Mems Accelerometer Seismic Accelerometer Capacitive Accelerometer Mems Accelerometer, Accelerometer Sensor Accelerometer Chip

US$ 190-210 / Piece
1 Piece  (MOQ)
MA1000A Very Low Noise Seismic Mems Accelerometer Main Features -Range:±2g~±30g, Excellent Bias Stability -Output: Differential Output / Single-Ended Output -Very Low Noise: 1.2μg/√Hz for ±2g Range (typical) -Input Power Supply: 4.75~5.25V -Embedded Self-Tes

Piezoelectric · Customized · Digital Output

Ahrs Heading Reference System Imu Sensor

US$ 550-1100 / Piece
10 Pieces  (MOQ)
Product Description Inertial Measurement Unit (IMU) Our IMU is a cost-effective high performance Attitude and Heading Reference System (AHRS). It contains the best in class magnetic calibration procedure for optimal heading, and It is suitable for low to medium dynamic applications. Fa

Capacitive · Non-Customized · Analog Output

Similar as Colibrys V1000 Accelerometer Module

US$ 190-210 / Piece
1 Piece  (MOQ)
MA1000A Very Low Noise Seismic Mems Accelerometer Main Features -Range:±2g~±30g, Excellent Bias Stability -Output: Differential Output / Single-Ended Output -Very Low Noise: 1.2μg/√Hz for ±2g Range (typical) -Input Power Supply: 4.75~5.25V -Embedded Self-Tes

Three · Customized · IP67

Fiber Optic Gyroscope Ins Strapdown Inertial Navigation System for Marine Navigation

US$ 6500-7000 / Piece
1 Piece  (MOQ)
Product Description INS-100 Industrial grade is a high-precision integrated navigation system. It is equipped with three self-developed 40 fiber optic gyroscopes, three-self MEMS accelerometers and GNSS modules, and realizes high-precision positioning and navigation in complex environments

Piezoresistive · CE · Analog Output

Honeywell HMS-MM-105613S Inertial Navigation Sensor for Autonomous Vehicles and Intelligent Robot

US$ 130-599 / Piece
1 Piece  (MOQ)
The Honeywell HMS-MM-105 series products are 6 degrees of freedom inertial measurement units. They feature high-precision and high-reliability MEMS tri-axis gyroscopes and tri-axis accelerometers, allowing for real-time measurement of angular velocity and acceleration of moving objects. Coupled with

Piezoelectric · Customized · Digital Output

Stim 300 Replacement Racing Ship Low Price Navigation Imu System

US$ 850-1100 / Piece
10 Pieces  (MOQ)
Product Description Inertial Measurement Unit (IMU) Our IMU is a cost-effective high performance Attitude and Heading Reference System (AHRS). It contains the best in class magnetic calibration procedure for optimal heading, and It is suitable for low to medium dynamic applications. Factory c

Capacitive · Non-Customized · Analog Output

Low Price Analog Mems Accelerometer

US$ 190-210 / Piece
1 Piece  (MOQ)
MA1000A series Low Price Analog MEMS Accelerometer Main Features -Range:±2g~±30g, Excellent Bias Stability -Output: Differential Output / Single-Ended Output -Very Low Noise: 1.2μg/√Hz for ±2g Range (typical) -Input Power Supply: 4.75~5.25V -Embedded Self-Te

Piezoelectric · Customized · Digital Output

Tactical Grade Integrated Mems Accelerometer and Gyroscope Attitude Sensing Inertial Measurement Unit

US$ 550-1100 / Piece
10 Pieces  (MOQ)
Product Description Inertial Measurement Unit (IMU) Our IMU is a cost-effective high performance Attitude and Heading Reference System (AHRS). It contains the best in class magnetic calibration procedure for optimal heading, and It is suitable for low to medium dynamic applications. Factory c

Capacitive · Non-Customized · Analog Output

China High Accuracy Mems Accelerometer

US$ 190-210 / Piece
1 Piece  (MOQ)
MA1000A series China High Accuracy MEMS Accelerometer Main Features -Range:±2g~±30g, Excellent Bias Stability -Output: Differential Output / Single-Ended Output -Very Low Noise: 1.2μg/√Hz for ±2g Range (typical) -Input Power Supply: 4.75~5.25V -Embedded Self

Capacitive · Non-Customized · Analog Output

Low Price Mems Accelerometer Sensor

US$ 190-210 / Piece
1 Piece  (MOQ)
MA1000A series Low Price MEMS Accelerometer Sensor Main Features -Range:±2g~±30g, Excellent Bias Stability -Output: Differential Output / Single-Ended Output -Very Low Noise: 1.2μg/√Hz for ±2g Range (typical) -Input Power Supply: 4.75~5.25V -Embedded Self-Te

Capacitive · Non-Customized · Analog Output

Chin Best Hot Selling Accelerometer Chip

US$ 190-210 / Piece
1 Piece  (MOQ)
MA1000A Very Low Noise Seismic Mems Accelerometer Main Features -Range:±2g~±30g, Excellent Bias Stability -Output: Differential Output / Single-Ended Output -Very Low Noise: 1.2μg/√Hz for ±2g Range (typical) -Input Power Supply: 4.75~5.25V -Embedded Self-Tes
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