Electronic Gyroscope Sensor
GSGYR203F Fiber Optic Gyroscope with Run-up Time 3s Bias Repeatability <0.5°/h and Bias Temperature Sensitivity <1°/h
GSGYR203F Fiber Optic Gyroscope Product Introduction The GSGYR203F is an inertial angular 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 between clockwise and counterclockwise light propagation in the fiber optic loop, which are induced by external angular velocity. The system converts these signals through
Low Power Consumption <3W Fibre Optic Gyroscope with Wide Operating Temperature -45°C～+70°C and Large Dynamic Range ±500°/s
GSGYR104F Fibre Optic Gyroscope Product Introduction This inertial angle rate sensor utilizes the optical Sagnac effect to measure rotational angular velocity along its sensitive axis. It employs a digital closed-loop detection circuit to extract optical path differences caused by external angular speed, modulating and demodulating voltage signals to achieve real-time angular velocity detection. Functionality Comprising an optical angular velocity sensitive unit and signal
GSGYR103F Fibre Optic Gyroscope with Digital Closed-Loop Detection All Solid State Design and Long Life for Precise Angular Velocity Measurement
GSGYR103F Fibre Optic Gyroscope Product Introduction This inertial angle rate sensor utilizes the optical Sagnac effect to measure rotational angular velocity along its sensitive axis. It employs a digital closed-loop detection circuit to extract optical path differences caused by external angular speed, modulating and demodulating voltage signals to achieve real-time angular velocity detection. Functionality Comprising an optical angular velocity sensitive unit and signal
GSGYR102F Fibre Optic Gyroscope with ±900°/s Dynamic Range All Solid State and Long Life for Inertial Navigation
GSGYR102F Fibre Optic Gyroscope Product Introduction The GSGYR102F 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 external physical angular speed, with voltage signal modulation and demodulation for real-time angular velocity detection. This gyroscope consists of two main components:
KSACC121Q Quartz Flexible Accelerometer for Inertial Navigation
KSACC121Q Quartz Flexible Accelerometer for Inertial Navigation Product Introduction The KSACC121Q Quartz Flexible Accelerometer is a precision instrument comprising quartz glass flexible support and advanced servo circuit based on the principle of inertia. When the carrier is subjected to acceleration, the output is precisely proportional to the input acceleration. Our accelerometer features a current output form with high output impedance, allowing users to select sampling
KSACC116Q Quartz Accelerometer ±80g Range 35g Weight
KSACC116Q Quartz Flexible Accelerometer ±80g Range 35g Weight Key Attributes Power Voltage ±12~±18V DC Weight ≤35g Size Ø18.2×23.6mm Resolution
KSACC115Q Quartz Flexible Accelerometer ±30g ±12-18V DC
KSACC115Q Quartz Flexible Accelerometer ±30g ±12~18V DC Product Overview The KSACC115Q Quartz Flexible Accelerometer is a precision instrument featuring quartz glass flexible support and advanced servo circuitry based on inertia principles. When subjected to acceleration, it provides output precisely proportional to input acceleration with high output impedance current output. Key Attributes Attribute Value Power Voltage ±12~±18V DC Input Range ±30g Bias ≤8mg Temperature
KSACC113Q Quartz Flexible Accelerometer ±80g Range for Inertial Navigation
KSACC113Q Quartz Flexible Accelerometer ±80g Range Key Attributes Power Voltage ±12~±18V DC Operating Temperature -45°C~+80°C Storage temperature -55°C～+80°C Shock 100g Vibration Peak Sine 20g@20Hz ~ 2000Hz Product Description The KSACC113Q Quartz Flexible Accelerometer is a precision instrument comprising quartz glass flexible support and advanced servo circuit based on the principle of inertia. When the carrier is subjected to acceleration, the output is precisely
KSACC112Q Quartz Flexible Accelerometer ±20g Range
KSACC112Q Quartz Flexible Accelerometer ±20g Range Product Attributes Attribute Value Power Voltage ±12~±18V DC Operating Temperature -45°C~+80°C Storage temperature -55°C～+80°C Shock 100g Vibration Peak Sine 15g@20Hz ~ 2000Hz Product Description KSACC112Q Quartz Flexible Accelerometer is a precision instrument comprising quartz glass flexible support and advanced servo circuit based on the principle of inertia. When the carrier is subjected to acceleration, the output is
KSACC111Q Quartz Flexible Accelerometer for Inertial Navigation
KSACC111Q Quartz Flexible Accelerometer for Inertial Navigation Product Introduction The KSACC111Q Quartz Flexible Accelerometer is a precision instrument featuring quartz glass flexible support and advanced servo circuitry based on inertia principles. When subjected to acceleration, it delivers output precisely proportional to input acceleration. This accelerometer features high output impedance current output, allowing users to select sampling resistance according to their
KSGYR101M MEMS Quartz Gyroscope Sensor 50Hz Bandwidth 5V DC
KSGYR101M MEMS Quartz Angular Rate Sensor 50Hz Bandwidth Key Attributes Attribute Value Input Voltage +5.0 Vdc Input Current < 8 mA @ +5.0 Vdc Scale Factor over Temperature < 0.1%/°C G Sensitivity (Typical) < 0.05°/sec/g Bandwidth (-3 dB) > 50 Hz Non-Linearity (% Full Range) < 0.05% Product Overview The KSGYR101M MEMS Quartz Angular Rate Sensor (Low Cost Gyro 50) features a MEMS (micro-electro-mechanical system) single-axis angular velocity sensor on a compact PC board. This
KSGYR301M MEMS Quartz Gyroscope ±100°/s Range 5Vdc
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
KSGYR312M Triaxial MEMS Gyro Sensor ±300°/s 5Vdc Product Attributes Input voltage 5Vdc Incoming current
KSGYR322M Three Axis Digital Gyro
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 MEMS Gyroscope ±300°/s Range High Precision
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 MEMS Gyro Chip ±400°/s SPI I2C
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
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 with ≤0.1°/h Bias, 71.5×68×45mm Dimensions, and <4W Power Dissipation
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 60x60x32mm +5V Supply
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)
KSGYR105F Fibre Optic Gyroscope 98×98×35mm -40°C～+70°C
KSGYR105F Fibre Optic Gyroscope Product Attributes Supply voltage +5V Dimensions 98×98×35mm Start time ≤5s Operate temperature -40°C～+70°C Weight