Three Axis Gyroscope
High Precision & Low Noise Three-Axis FOG SIS-100HD, 0.005°/h Zero Bias Stability, High Reliability for INS & AHRS Systems
The product is an inertial angular velocity sensor based on the Sagnac effect for measuring the rotational angular velocity of the carrier along the sensitive axis. The digital closed-loop detection circuit is used to extract the optical path difference of the counterclockwise propagating light caused by the external physical angular speed of the optical fiber coil. At the same time, the voltage signal of the optical path difference signal is converted to modulation and
High Precision & Low Noise Three-Axis Gyroscope SIS-70A, 0.05°/h Zero Bias Stability, High Reliability for UAV, Aircraft & Ship Navigation
The product is an inertial angular velocity sensor based on the Sagnac effect for measuring the rotational angular velocity of the carrier along the sensitive axis. The digital closed-loop detection circuit is used to extract the optical path difference of the counterclockwise propagating light caused by the external physical angular speed of the optical fiber coil. At the same time, the voltage signal of the optical path difference signal is converted to modulation and
SIS‑40 3‑Axis Integrated FOG | Ultra‑Compact 71.5×71.5×47 mm, 0.1°/h Zero‑Bias Stability, High‑Reliability for Marine & Inertial Navigation
The product is an inertial angular velocity sensor based on the Sagnac effect for measuring the rotational angular velocity of the carrier along the sensitive axis. The digital closed-loop detection circuit is used to extract the optical path difference of the counterclockwise propagating light caused by the external physical angular speed of the optical fiber coil. At the same time, the voltage signal of the optical path difference signal is converted to modulation and
SIS-100 3-Axis FOG with 0.05°/h Zero-Bias Stability and High Precision North Finder Gyro for Digital Closed-Loop Detection
SIS-100 3-Axis FOG delivers ≤0.05°/h bias stability with 500Hz bandwidth. Custom OEM/ODM support, -45℃ to +70℃ operating range, and 1-year warranty for motion sensing, stabilization, and navigation applications.
High Precision & High Reliability Triple-Axis FOG SIS-120D, 0.005°/h Zero Bias Stability for Precision Stabilized Platforms, North Finders & INS
The product is an inertial angular velocity sensor based on the Sagnac effect for measuring the rotational angular velocity of the carrier along the sensitive axis. The digital closed-loop detection circuit is used to extract the optical path difference of the counterclockwise propagating light caused by the external physical angular speed of the optical fiber coil. At the same time, the voltage signal of the optical path difference signal is converted to modulation and
High Precision Triple-Axis FOG SIS-120C | 0.005°/h Zero Bias Stability, High Stability for INS & UAV Navigation
The product is an inertial angular velocity sensor based on the Sagnac effect for measuring the rotational angular velocity of the carrier along the sensitive axis. The digital closed-loop detection circuit is used to extract the optical path difference of the counterclockwise propagating light caused by the external physical angular speed of the optical fiber coil. At the same time, the voltage signal of the optical path difference signal is converted to modulation and
Ultra-High Precision Three-Axis FOG SIS-120H, 0.003°/h Zero Bias Stability for High-End INS & Attitude Measurement Systems
The product is an inertial angular velocity sensor based on the Sagnac effect for measuring the rotational angular velocity of the carrier along the sensitive axis. The digital closed-loop detection circuit is used to extract the optical path difference of the counterclockwise propagating light caused by the external physical angular speed of the optical fiber coil. At the same time, the voltage signal of the optical path difference signal is converted to modulation and
High Precision & Low Noise Three-Axis FOG SIS-100, 0.01°/h Zero Bias Stability, High Reliability for INS & AHRS Systems
The product is an inertial angular velocity sensor based on the Sagnac effect for measuring the rotational angular velocity of the carrier along the sensitive axis. The digital closed-loop detection circuit is used to extract the optical path difference of the counterclockwise propagating light caused by the external physical angular speed of the optical fiber coil. At the same time, the voltage signal of the optical path difference signal is converted to modulation and
High Precision Three-Axis FOG SIS-90H, 0.01°/h Zero Bias Stability for North Finders & Inertial Navigation Systems
The product is an inertial angular velocity sensor based on the Sagnac effect for measuring the rotational angular velocity of the carrier along the sensitive axis. The digital closed-loop detection circuit is used to extract the optical path difference of the counterclockwise propagating light caused by the external physical angular speed of the optical fiber coil. At the same time, the voltage signal of the optical path difference signal is converted to modulation and
SIS‑40 3‑Axis Integrated FOG | 0.1°/h Zero‑Bias Stability | Ultra Compact Marine Navigation Gyro
This fiber-optic gyroscope is a high-precision inertial angular rate sensor based on the Sagnac effect, designed to measure the rotational angular velocity of a carrier along the sensitive axis. It adopts a digital closed-loop detection circuit to capture the optical path difference of counter-propagating light inside the fiber coil induced by external rotational motion. The system converts the optical path difference into a voltage signal, and completes signal modulation and
High Precision & Low Noise Three-Axis FOG SIS-100HD, 0.005°/h Zero Bias Stability, High Reliability for INS & AHRS Systems
This fiber‑optic gyroscope is an inertial angular velocity sensor built upon the Sagnac effect, which measures the carrier’s rotational angular velocity along the sensitive axis. Adopting a digital closed‑loop detection circuit, it captures the optical‑path difference of counter‑propagating light inside the fiber coil induced by external rotational angular velocity. The optical‑path difference is converted into a voltage signal for modulation and demodulation. Closed‑loop
SIS‑100 3‑Axis Fiber Optic Gyroscope | 0.05°/h Zero‑Bias Stability, High‑Precision for North Finder & Inertial Navigation Systems
This fiber‑optic gyroscope is an inertial angular‑rate sensor based on the Sagnac effect, which measures the carrier’s rotational angular velocity along the sensitive axis. Equipped with a digital closed‑loop detection circuit, it captures the optical path difference of counter‑propagating light inside the fiber coil induced by external rotation. The optical‑path‑difference signal is converted into voltage signal, followed by signal modulation‑demodulation and closed‑loop