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HTS- AHRS-93A Attitude and Heading Reference System

HTS- AHRS-93A Attitude and Heading Reference System

HTS- AHRS-93A Attitude and Heading Reference System (AHRS) features a unique solid-state design that is compact and lightweight. Embedded a cost-effective MEMS gyroscopes, high precison MEMS accelerometers, magnetometers and barometers ensure high reliability and low power consumption. Continuous monitoring of all functions and internal diagnostics gives you a high integrity system.
HTS- AHRS-92A Attitude and Heading Reference System

HTS- AHRS-92A Attitude and Heading Reference System

HTS- AHRS-92A Attitude and Heading Reference System (AHRS) features a unique solid-state design that is compact and lightweight. Embedded a cost-effective MEMS gyroscopes, high precison MEMS accelerometers, magnetometers and barometers ensure high reliability and low power consumption. Continuous monitoring of all functions and internal diagnostics gives you a high integrity system.

HTS- AHRS-91A Attitude and Heading Reference System

HTS- AHRS-91A Attitude and Heading Reference System

The HTS-AHRS-91A Attitude and Heading Reference System is MEMS based inertial system designed to provide accurate orientation and motion data in dynamic environments. The system uses advanced sensor fusion algorithms, combined with accelerometers, gyroscopes and magnetometers, to provide accurate real-time attitude, heading and angular rate measurements. Which is an ideal solution for aviation, marine, robotics and unmanned system applications.
HTS-AHRS-62 Attitude and Heading Reference System

HTS-AHRS-62 Attitude and Heading Reference System

HTS-AHRS-62 Attitude and Heading Reference System consists of a MEMS inertial measurement unit, a unique heading attitude algorithm and a complementary filtering algorithm. The system uses MEMS device temperature error compensation technology and complementary filtering algorithms to maintain attitude accuracy for a long time, adapt to complex environments with high dynamics and high overload, and output stable and reliable attitude information in dynamic environments.
HTS-AHRS-67 Attitude and Heading Reference System

HTS-AHRS-67 Attitude and Heading Reference System

The HTS-AHRS-67 Attitude and Heading Reference System is MEMS based inertia system designed to provide accurate orientation and motion data in dynamic environments. The system uses advanced sensor fusion algorithms, combined with accelerometers, gyroscopes and magnetometers, to provide accurate real-time attitude, heading and angular rate measurements. Which is an ideal solution for aviation, marine, robotics and unmanned system applications.

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