Electronic Gyroscope Sensor
Inertial Navigation Systems Angular Velocity Measuring Instrument With Random Walk Coefficient≤0.01(º)/H^1/2
Product Description: This product is an inertial angle rate sensor based on the optical 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 clockwise light caused by the external physical angular speed, and the voltage signal of the optical path signal is modulated and demodulation, and the closed loop feedback and control are
≤0.01(º)/h^1/2 Random Walk Coefficient Electronic Gyroscope Sensor For Precise Measurement
Product Description: This product operates as an inertial angle rate sensor based on the optical Sagnac effect, measuring the rotational angular velocity of the carrier along its sensitive axis. Employing a digital closed-loop detection circuit, it extracts the optical path difference resulting from external physical angular speed in the clockwise direction. Modulation and demodulation of the voltage signal from the optical path enable closed-loop feedback and control,
Optical angular velocity sensors are used in aerospace, Dynamic range ±900 (°) / s,weight ＜130(g)
Product Description: Based on the optical Sagnac effect, this device functions as an inertial angle rate sensor designed to measure the rotational angular velocity of the carrier along its sensitive axis. It utilizes a digital closed-loop detection circuit to extract the optical path difference caused by external physical angular speed in the clockwise direction. Modulating and demodulating the voltage signal from the optical path enable closed-loop feedback and control,
Fiber Optic Gyroscope Sensor with ±500 (°)/s Dynamic Range, -45～+70 (℃) Operate Temperature and RS422 Digital Output
Product Description: This product is an inertial angle rate sensor based on the optical 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 clockwise light caused by the external physical angular speed, and the voltage signal of the optical path signal is modulated and demodulation, and the closed loop feedback and control are
Miniaturized Three-Axis Fiber Optic Gyroscope with RS422 Interface and Low Bias Drift
Product Description: This product is an inertial angle rate sensor based on the optical 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 clockwise light caused by the external physical angular speed, and the voltage signal of the optical path signal is modulated and demodulation, and the closed loop feedback and control are
Fiber Optic Gyroscope with Random Walk Coefficients ≤0.01(°/h1/2) RS422 Digital Output for Inertial Navigation Systems
Product Description: This product is an inertial angle rate sensor based on the optical 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 clockwise light caused by the external physical angular speed, and the voltage signal of the optical path signal is modulated and demodulation, and the closed loop feedback and control are
Automotive navigation grade fiber optic gyroscope with ≤0.1(°)/h Bias drift and weight≤320(g)
Product Description:This product is an inertial angle rate sensor based on the optical 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 clockwise light caused by the external physical angular speed, and the voltage signal of the optical path signal is modulated and demodulation, and the closed loop feedback and control are
Three axis fiber optic gyroscope for flight attitude detection Digital output and weight ≤320(g)
Product Description: This product is an inertial angle rate sensor based on the optical 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 clockwise light caused by the external physical angular speed, and the voltage signal of the optical path signal is modulated and demodulation, and the closed loop feedback and control are
Airborne fiber optic gyroscope is used for attitude detection with Bias drift ≤0.1(°)/h and ±500 (°)/s Dynamic range
Product Description:This product is an inertial angle rate sensor based on the optical 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 clockwise light caused by the external physical angular speed, and the voltage signal of the optical path signal is modulated and demodulation, and the closed loop feedback and control are
Three axis fiber optic gyroscope for IMU with Bias drift ≤0.1(°) /h and weight＜320(g)
Product Description: This product is an inertial angle rate sensor based on the optical 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 clockwise light caused by the external physical angular speed, and the voltage signal of the optical path signal is modulated and demodulation, and the closed loop feedback and control are
High Precision Electronic Gyroscope Sensor With Bandwidth 500Hz Bias Repeatability ≤0.5/≤1°/H
Product Description: The KSFG3X36-1 fiber optic gyro, as illustrated in the figure, is a low-precision three-axis gyro featuring a compact design, lightweight structure, lack of moving components, high reliability, and extended lifespan. Its digital output is conveniently integrated with systems, making it applicable in aviation, aerospace, naval operations, defense, coal mine measurements, automotive electronics, and other varied fields. Based on optical principles, the
High Precision Fiber Optic Gyroscope Used For Strapdown Inertial Navigation And Aircraft Navigation
KSFG-120series Gyro This product is an inertial angle rate sensor based on the optical 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 clockwise light caused by the external physical angular speed, and the voltage signal of the optical path signal is modulated and demodulation, and the closed loop feedback and control are
High Precision Fiber Optic Gyroscope with 120×120×38 mm Dimensions and -45～+70°C Operate Temperature for Inertial Measurement
KSFG-120series Gyro This product is an inertial angle rate sensor based on the optical 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 clockwise light caused by the external physical angular speed, and the voltage signal of the optical path signal is modulated and demodulation, and the closed loop feedback and control are
Inertial Navigation Systems Electronic Gyroscope Sensor Based On Optical Sagnac Effect
KSFG-98series Gyro This product is an inertial angle rate sensor based on the optical 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 clockwise light caused by the external physical angular speed, and the voltage signal of the optical path signal is modulated and demodulation, and the closed loop feedback and control are realized
Inertial Navigation Grade Electronic Gyroscopes Used In Measurement Units And Systems
Inertial Navigation Grade Electronic Gyroscopes Used In Measurement Units And Systems This product is an inertial angle rate sensor based on the optical 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 clockwise light caused by the external physical angular speed, and the voltage signal of the optical path signal is modulated and
70×70×32 mm Optical Gyroscope with 5s Start Time and -40～+70℃ Operate Temperature for Inertial Navigation Systems
KSFG-70series Gyro This product is an inertial angle rate sensor based on the optical 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 clockwise light caused by the external physical angular speed, and the voltage signal of the optical path signal is modulated and demodulation, and the closed loop feedback and control are realized
High Precision Digital Optical Gyroscope with 70×70×32 mm Dimensions and -40℃～+70℃ Operating Temperature for UAV Navigation
K1FOG40 series Gyro This product is an inertial angle rate sensor based on the optical 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 clockwise light caused by the external physical angular speed, and the voltage signal of the optical path signal is modulated and demodulation, and the closed loop feedback and control are
High Precision Fiber Optic Gyroscopes Used In Inertial Measurement Units，Bias drift ≤0.1 (°) / h
K1FOG20 series Gyro This product is an inertial angular rate sensor that utilizes the optical Sagnac effect to measure the rotational angular velocity of the carrier along its sensitive axis. It employs a digital closed-loop detection circuit to capture the optical path difference in clockwise light caused by external angular velocity. The optical path voltage signal is modulated and demodulated, with closed-loop feedback and control, enabling real-time detection of angular
Navigation Grade Fiber Optic Gyroscope Used In Inertial Navigation Systems，Dimensions 50×50×36 (mm)
K1FOG20 series Gyro This product is an inertial angular rate sensor that operates based on the optical Sagnac effect, designed to measure the rotational angular velocity of a carrier along its sensitive axis. It uses a digital closed-loop detection circuit to capture the optical path difference in the clockwise light caused by external angular velocity. The system modulates and demodulates the voltage signal from the optical path, enabling real-time feedback and control in
Lidar Cloud Map Matching And Environment Sensing Devices For Driverless Car Navigation
KsINS-L LiDAR point cloud map matching and environment sensing equipment product description: Based on inertial navigation information, satellite navigation information and liDAR/camera information, the liDAR point cloud map matching and environment sensing equipment can realize the functions of high-precision map matching and positioning, online precision mapping, typical target identification and tracking and relative distance measurement, etc., with high accuracy, strong