Electronic Gyroscope Sensor

KSGYR301M MEMS Quartz Gyroscope ±100°/s Range 5Vdc Product Overview The KSGYR301M MEMS Quartz Gyroscope utilizes advanced quartz MEMS technology to measure angular velocities across multiple axes (configurable to customer requirements), with digital output via serial port. Key Specifications Attribute Value Input Voltage 5±0.2 Vdc Input Current < 50 mA Measurement range ±100°/s Bias ≤0.03°/s Bias stability ≤20°/h Bias repeatability ≤20°/h Product Features Mass production

KSGYR312M Triaxial MEMS Gyro Sensor ±300°/s 5Vdc Product Attributes Input voltage 5Vdc Incoming current

KSGYR311M Triaxial Universal Angular Rate Gyro Product Specifications Attribute Value Input voltage 6-15Vdc Incoming current

KSGYR322M Three Axis Digital Gyro Product Attributes Attribute Value Input voltage 5V DC Power dissipation ≤1W @5V DC Range ±500(triaxial)°/s Bias ≤±0.1°/s(In 500°/s) Bias stability ≤0.5°/h(Allan deviation) Bias repeatability ≤0.05°/s Size 45×39×20mm Product Description KSGYR322M Three Axis Digital Gyro Product Introduction KSGYR322M series solid state angular rate sensor (gyro) measures angular rate using micromechanoelectronic system (MEMS) technology chips. Manufactured

KSGYR321M High Precision MEMS Gyroscope ±300°/s Range Key Specifications Attribute Value Range (°/s) ±300 (options) Bias stability (deg/h, allan deviation) ≤12 Bias repeatability (deg/s) ≤0.15 Nonlinearity (%F.R) ≤0.1 Resolution (deg/s) ≤0.05 Bandwidth (Hz) ≥80 Product Overview The KSGYR321M is a high-performance three-axis digital gyroscope featuring compact size and exceptional overload resistance. Designed for precision navigation, control systems, and dynamic measurement

KSGYR111M-S Digital Quartz MEMS GYRO Chip Key Attributes Attribute Value Supply voltage VDDM +2.7V~+3.6V Bias ZRL ±1°/s (0 LSB Typ) Rate range I ±400°/s Non-linearity NI ±0.5%FS Cross-axis sensitivity CS ±5% Product Overview The KSGYR111M-S Digital Quartz MEMS GYRO Chip features superior bias output stability and low noise. This digital quartz gyroscope is based on quartz MEMS technology and manufactured using semiconductor processing techniques. Key Features Excellent bias

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

KSGYR312F Three Axis Fiber Optic Gyroscope The KSGYR312F 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 optical path differences caused by external physical angular speed, enabling real-time angular velocity signal detection through modulation, demodulation, and closed-loop feedback control. Product

KSGYR103F Fibre Optic Gyroscope Key Specifications Attribute Value Supply voltage +5(V) Dimensions 60×60×32 mm Start time ≤3 s Bias stability (10s smooth -45°C~+70°C) ≤0.5 °/h Power dissipation (full temperature)

KSGYR106F Series Gyro Sensor for Inertial Navigation Systems Product Overview The KSGYR106F Series is an inertial angle rate sensor based on the optical Sagnac effect, designed to measure rotational angular velocity along its sensitive axis. This advanced sensor utilizes a digital closed-loop detection circuit to precisely extract optical path differences caused by external physical angular speed, enabling real-time angular velocity signal detection. Key Attributes Attribute

KSGYR105F Fibre Optic Gyroscope Product Attributes Supply voltage +5V Dimensions 98×98×35mm Start time ≤5s Operate temperature -40°C～+70°C Weight

KSGYR104F Fibre Optic Gyroscope Product Overview The KSGYR104F is an inertial angle rate sensor based on the optical Sagnac effect, designed to measure rotational angular velocity along the sensitive axis. It utilizes a digital closed-loop detection circuit to extract optical path differences caused by external angular velocity, providing precise real-time angular velocity signal detection. Key Attributes Attribute Value Supply voltage +5V Dimensions 70×70×32 mm Start time 5s

KSGYR102F Fibre Optic Gyroscope 50x50x36mm +5V Product Attributes Attribute Value Supply voltage +5 V Dimensions 50×50×36 mm Start time 5 s Bias repeatability ≤0.05 °/h Operate temperature -45°C～+70°C Product Description The KSGYR102F is an inertial angle rate sensor based on the optical Sagnac effect, designed to measure rotational angular velocity along its sensitive axis. It utilizes a digital closed-loop detection circuit to extract optical path differences caused by

KFOIMUm Inertial Navigation System Specification Product Description: KFOIMUm series inertial navigation system is a typical shelf product. With high-performance fiber optic gyro and accelerometer, KFOIMUm series inertial navigation can meet the needs of autonomous navigation in complex environments, and can integrate satellite, Doppler, odometer and other information to achieve high-precision integrated navigation. Series products have been widely used in defense,

KFOIMUm Inertial Navigation System Specification Product Description: KFOIMUm series inertial navigation system is a typical shelf product. With high-performance fiber optic gyro and accelerometer, KFOIMUm series inertial navigation can meet the needs of autonomous navigation in complex environments, and can integrate satellite, Doppler, odometer and other information to achieve high-precision integrated navigation. Series products have been widely used in defense,

KFOIMUm Inertial Navigation System Specification Product Description: KFOIMUm series inertial navigation system is a typical shelf product. With high-performance fiber optic gyro and accelerometer, KFOIMUm series inertial navigation can meet the needs of autonomous navigation in complex environments, and can integrate satellite, Doppler, odometer and other information to achieve high-precision integrated navigation. Series products have been widely used in defense,

KFOIMUH Inertial Navigation System Specification Product Description: KFOIMUH series inertial navigation system is a typical shelf product. With high-performance fiber optic gyro and accelerometer, KFOIMUH series inertial navigation can meet the needs of autonomous navigation in complex environments, and can integrate satellite, Doppler, odometer and other information to achieve high-precision integrated navigation. Series products have been widely used in defense,

KFOIMUH Inertial Navigation System Specification Product Description: KFOIMUH series inertial navigation system is a typical shelf product. With high-performance fiber optic gyro and accelerometer, KFOIMUH series inertial navigation can meet the needs of autonomous navigation in complex environments, and can integrate satellite, Doppler, odometer and other information to achieve high-precision integrated navigation. Series products have been widely used in defense,

KFOIMUH Inertial Navigation System Specification Product Description: KFOIMUH series inertial navigation system is a typical shelf product. With high-performance fiber optic gyro and accelerometer, KFOIMUH series inertial navigation can meet the needs of autonomous navigation in complex environments, and can integrate satellite, Doppler, odometer and other information to achieve high-precision integrated navigation. Series products have been widely used in defense,

Product Description: KQ6IMU100 is a highly advanced inertial measurement module that has been developed using the latest MEMS technology. With its exceptional measurement capabilities, this module can accurately measure the angular velocity and acceleration of the carrier in three different directions. MEMS technology is a revolutionary micro-device system that integrates various micro-components such as micro-sensors, micro-actuators, micro-mechanical structures, power and