Electronic Gyroscope Sensor
Gyroscope/Angular velocity sensor/Used to measure the angular velocity in the direction of the sensitive axis
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 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
Small Lightweight High Reliability Three Axis Gyroscopes Used In Industry And Aerospace
KSFG-3X36 three-axis series gyro KSFG3X36-1 fiber optic gyro is a low-precision three-axis gyro, as shown in Figure 1, with the advantages of small volume, light weight, no moving parts, high reliability, long life, etc. Its digital output is convenient and integrated with the system, which can be applied to aviation, aerospace, ships, weapons, coal mine measurement, automotive electronics and other fields. The fiber optic gyroscope principle is an inertial navigation
Light Weight Small Size High-precision Kacise Flexible Dynamically Tuned Gyroscope for Aerospace with Shock ≥50g
Light Weight Small Size High-precision Kacise Flexible Dynamically Tuned Gyroscope for Aerospace Feature Light weight Small size Long service life Wide dynamic range High reliability Wide application and etc. Introduction KTG-30 has been used in ship navigation, artillery and other systems to quickly find north. Parameter Parameter Spec. Vaule Unit Power Power(3 Phase) 20&500 V & Hz Power(1 Phase) 7&16000 V & Hz performance Random Drift ≤0.03 °/h Drift stability ≤0.2 °/h Non
Inertial Angular Velocity Sensor For Photoelectric Pod Flight Control Platform
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