Electronic Gyroscope Sensor
Light Weight <130g Inertial Optical Gyroscope with Operate Temperature -45℃～+70℃ and Random Walk Coefficient ≤0.01º/h^1/2 for UAVs
Product Description: Operating on the optical Sagnac effect, this product serves as an inertial angle rate sensor designed to measure the rotational angular velocity of the carrier along its sensitive axis. A digital closed-loop detection circuit is utilized to capture the optical path difference caused by external physical angular speed in the clockwise direction. Modulating and demodulating the voltage signal from the optical path facilitate closed-loop feedback and control
≤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
High-precision Three-axis FOG Sensor for UAV Navigation with Weight <320g 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
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
Inertial Angular Rate Sensor with ≤0.1°/h Bias Drift Compact 50×50×36mm and 5s Start Time
K1FOG20 series Gyro 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
GSGYR112F Single-Axis Fiber Optic Gyroscope with 60×60×30mm Size, RS422 Output, and 1s Run-up Time
GSGYR112F Single-Axis Fiber Optic Gyroscope Product Overview The GSGYR112F single-axis fiber optic gyroscope series features an all-digital closed-loop operating mode with excellent characteristics including small size, light weight, low power consumption, fast startup, and simple interface. This high-precision angular rate sensor is ideal for navigation and control applications, widely used in various control and braking fields. Key Features Single 5V power supply Excellent
GSGYR106F Single-axis Fiber Optic Gyroscope with Digital Closed-Loop Detection, Instant Start, and Low Bias for Precision Angular Velocity Measurement
GSGYR106F Single-axis Fiber Optic Gyroscope Product Introduction This product is an inertial angle rate sensor based on the optical Sagnac effect, designed to measure the rotational angular velocity of the carrier along the sensitive axis. It utilizes a digital closed-loop detection circuit to extract the optical path difference of clockwise light caused by external physical angular speed. The system modulates and demodulates the voltage signal of the optical path, achieving
GSGYR105F Fibre Optic Gyroscope with ±500°/s Dynamic Range 3s Start Time and <4W Power Dissipation
GSGYR105F Fibre Optic Gyroscope Product Introduction 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 extracts the optical path difference of the clockwise light caused by external physical angular speed, modulates and demodulates the voltage signal of the optical path signal, and implements closed-loop feedback and
Electronic Gyroscope Sensor with ≤0.01/≤0.1 Random Walk Coefficients and Reliable Performance in Compact Form Factor
≤0.01/≤0.1 Random Walk Coefficients Electronic Gyroscope Sensor Reliable Performance Product Overview The KSFG3X36-1 fiber optic gyro is a three-axis gyro with low precision, featuring a compact form factor, lightweight build, absence of moving parts, high reliability, and extended lifespan. Its digital output enables easy system integration for applications in aviation, aerospace, maritime, defense, coal mine measurements, automotive electronics, and diverse fields. Based on
GSGYR131M Single Axis Digital Gyro Sensor with ±75°/s Range ≤15°/h Bias Stability and ≤1°/s Bias Temperature Sensitivity
GSGYR131M Single Axis Digital GYRO Sensor The GSGYR131M single-axis digital quartz gyroscope measures angular velocity information in real time for carriers including combat vehicles, UAVs, and aerial bombs. Designed for inertial navigation, flight control, and attitude stabilization systems, it is widely used across petroleum, coal, water resources, automotive, marine, and aviation industries. The gyroscope operates on the principle that quartz deformation during rotation
KSACC101Q Quartz Accelerometer ±70g 400Hz Digital Output
KSACC101Q Quartz Accelerometer ±70g 400Hz Digital Output Product Attributes Attribute Value Input Voltage 15±1 VDC Power consumption ≤75mW @15VDC Range ±70g Scale factor 56Hz/g±5Hz/g Scale factor repeatability(1σ,one month) ≤50ppm Bandwidth ≥400Hz Product Description The KSACC101Q quartz vibration beam accelerometer is a solid-state digital output acceleration sensor featuring large range, compact size, high precision, low power consumption, fast start-up time, shock
KSGYR131M Single Axis Digital Gyro Sensor ±75°/s Range
KSGYR131M Single Axis Digital Gyro Sensor ±75°/s Range Key Specifications Attribute Value Power Voltage +6V~+20V DC Turn-on time ≤2s Range ±75°/s Bias 0°/s±1°/s Bias stability(1σ)@25°C ≤15°/h Operating temperature -40°C～+85°C Product Overview The KSGYR131M single-axis digital quartz gyroscope measures angular velocity information in real time for carriers including combat vehicles, UAVs, and aerial bombs. Ideal for inertial navigation, flight control, and attitude stabilizati
≤1 W 5V DC Power Dissipation Mems Gyroscope For Intelligent Automobile
Product Description: The KS3ARG02D series solid state angular rate sensor, commonly referred to as a gyro, is engineered to measure the angular rate with great precision. It incorporates advanced microelectromechanical system (MEMS) technology, ensuring cutting-edge performance and accuracy. Renowned for its manufacturing, the sensor employs a sophisticated bipolar metal oxide semiconductor (BIMOS) technology during its production process. Additionally, it boasts an
GSGYR324F All-Solid-State Digital Closed-Loop Three-Axis Fiber Optic Gyroscope with Single 5V Power Supply and Bias Stability <0.5°/h
GSGYR324F Fiber Optic Gyroscope Product Introduction The GSGYR324F is an all-solid-state digital closed-loop three-axis integrated fiber optic gyroscope. Based on the Sagnac principle, it consists of an SLD light source, fiber optic coupler, photodetector, integrated optical phase modulator, fiber optic sensing coil, circuit, and structural body. Available in both integrated and split configurations, this three-axis fiber optic gyroscope is specifically designed for