The KT-EX6-7 micro inertial measurement unit consists of a cost-effective MEMS gyroscope chip and a MEMS accelerometer chip and its drive pickup circuit, temperature sensor, digital signal processing circuit and software, etc. It is used to measure the three-axis angular velocity and three-axis acceleration of the carrier in real time. The product adopts its own miniaturized, earthquake-resistant, impact-resistant structural design and flexible connection technology. The software has built-in full-temperature compensation, installation misalignment angle compensation, nonlinear compensation and other algorithms to ensure that the product can maintain stable performance under harsh environmental conditions such as static, dynamic, large impact, and high overload. It also outputs reliable six-degree-of-freedom measurement data after error compensation to users through the RS-422 serial port.

The KT-EX7-2 attitude measurement unit consists of a domestic three-axis gyroscope, a domestic three-axis accelerometer, a temperature sensor, a signal processing board, a structure and necessary software. It is used to measure the three-axis angular rate, three-axis acceleration and horizontal attitude angle (including pitch angle and roll angle) of the moving carrier. The attitude is output through algorithms such as the 9th-order Kalman filter and in accordance with the agreed communication protocol. Attitude angle information and inertial navigation information.

KT-EX6-17 is a highly integrated high-performance attitude measurement unit designed specifically for navigation and control applications. It consists of a three-axis gyroscope, a three-axis meter, a temperature sensor, a signal processing board, a structure and necessary software. Through the RS-422 serial port, it outputs the carrier heading and attitude accuracy after error compensation (including temperature compensation, installation misalignment angle compensation, nonlinear compensation, etc.) according to the agreed communication protocol.

The KT-EX5-1 dual-axis attitude sensor consists of a dual-axis attitude sensor, a temperature sensor, a signal processing board, a structure and necessary software. It is used to measure the horizontal attitude angle of the carrier and output the horizontal attitude angle information after error compensation (including temperature compensation, nonlinear compensation, etc.) through the RS-422 serial port according to the agreed communication protocol.

The KT-EX6-15 micro inertial measurement unit consists of a three-axis gyroscope, a three-axis meter, a temperature sensor, a signal processing board, a structure and necessary software. It is used to measure the three-axis angular rate and acceleration of the carrier, and outputs three angular rates, three acceleration data and temperature values ​​after error compensation (including temperature compensation, installation misalignment angle compensation, nonlinear compensation, etc.) through the RS-422 serial port according to the agreed communication protocol.

The KT-EX6-10 inertial measurement unit consists of a three-axis gyroscope, a three-axis meter, a temperature sensor, a signal processing board, a structure and necessary software. It is used to measure the three-axis angular rate and acceleration of the carrier, and outputs three angular rates and three acceleration data after error compensation (including temperature compensation, installation misalignment angle compensation, nonlinear compensation, etc.) through the RS-422 serial port according to the agreed communication protocol.

The KT-EX6-13 micro inertial measurement unit consists of domestic MEMS gyroscope chip and MEMS accelerometer chip and its drive pickup circuit, temperature sensor, digital signal processing circuit and software, etc., and is used to measure the three-axis angular velocity and three-axis acceleration of the carrier in real time. The product adopts its own anti-seismic and impact-resistant structural design and flexible connection technology. The software has built-in full-temperature compensation, installation misalignment angle compensation, nonlinear compensation and other algorithms to ensure that the product can maintain stable performance under static and dynamic as well as harsh environmental conditions, and output reliable six-degree-of-freedom measurement data after error compensation to users through the RS-422 serial port.

KT-EX9-2 is an inertial measurement unit (IMU) based on micro-electromechanical technology (MEMS). The system consists of a built-in three-axis MEMS gyroscope, a three-axis MEMS accelerometer, a three-axis magnetometer and an atmospheric pressure sensor, as well as its drive pickup circuit, temperature sensor, digital signal processing circuit, structure and software. The product adopts its own structural design, and the software has built-in full-temperature compensation, installation misalignment angle compensation, nonlinear compensation and other algorithms to ensure that the product can maintain stable performance under static and dynamic conditions and harsh environmental conditions, and provide users with reliable measurement data.