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Built with MEMS, quartz and fiber optic sensing cores, these devices deliver ultra-stable output, low bias drift, high resolution and outstanding linearity, paired with robust temperature compensation and strong shock/vibration resistance. Compact lightweight structures support fast boot-up, analog and digital signal interfaces, and multi-tier precision options to fit diverse accuracy demands. They enable angular velocity, linear acceleration and geomagnetic field measurement, supporting standalone sensing and combined positioning with GNSS, DVL and odometer data fusion. Widely applied in gimbal stabilization, aerospace flight control, marine navigation, industrial vibration testing and defense positioning.
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GSACC101M delivers high-sensitivity single-axis vibration sensing with ±1g range and 1000mV/g analog output. Resolution better than 0.001g and nonlinearity ≤0.5%FS ensure accurate low-frequency acceleration measurement. The 19.5×18.8×8.4mm package draws just 2mA from a 5V supply with full temperature compensation. Designed for flight control stabilization and seismic detection where precision at low frequencies is critical.
GSINS025C achieves attitude
GSINS016C integrates high-performance FOG and quartz accelerometers within a 110×110×100mm, 1.6kg compact chassis. Heading alignment accuracy better than 0.1° (1σ) with pure inertial navigation better than 2nm/h (CEP). Supports GNSS, DVL, and odometer data fusion for enhanced positioning resilience. Built for naval, land, aviation, and defense applications where size and weight matter without sacrificing accuracy.
GSTIM300 delivers 0.5°/h gyro bias stability in a MEMS design that meets general military standards. RS-422 interface supports 500Hz high-speed data output, while 5000g shock tolerance and -45°C to +85°C operation ensure survival in extreme environments. Integrated attitude solving (pitch/roll) reduces external processing needs. M4 screw mounting provides secure mechanical integration for guided weaponry, aviation stabilization, and dynamic measurement tasks.
GS16488 combines 3-axis gyro, accelerometer, magnetometer, and barometer into a true 10-DOF inertial solution. With gyro bias 0.5°/h and accelerometer bias 10μg, it delivers precision previously found only in larger systems. The 44×47×14mm package supports SPI interface and operates from -40°C to +85°C. Designed as a drop-in replacement for imported IMUs, it serves gimbal stabilization, rail inspection, and UAV navigation with uncompromised performance.
GSMTI3 is a self-contained Attitude Heading and Reference System (AHRS). This fully functional self-contained module can be easily designed by adding limited hardware components.
Since 2008, Gyrosens has been committed to delivering reliable and accurate motion sensing and navigation products, including gyroscopes, accelerometers, IMUs (Inertial Measurement Units), and AHRS (Attitude and Heading Reference Systems).
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