Electronic Gyroscope Sensor
KSACC117Q Quartz Flexible Accelerometer ±10g Range DC Power
KSACC117Q Quartz Flexible Accelerometer ±10g Range Product Attributes Attribute Value Power Voltage ±12~±18V DC Input Range ±10g Bias ≤10mg Temperature Sensitivity ≤100μg/°C Three-hour Stability(1σ) ≤100μg Scale Factor 2.3 ~ 3.5mA/g Product Description KSACC117Q Quartz Flexible Accelerometer 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
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
KSACC114Q Quartz Flexible Accelerometer ±20g Range ≤70g
KSACC114Q Quartz Flexible Accelerometer Product Attributes Attribute Value Power Voltage ±12~±18V DC Weight ≤70g Size Ø25.4×32mm Resolution
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
KSGYR311M Triaxial Universal Angular Rate Gyro
KSGYR311M Triaxial Universal Angular Rate Gyro Product Specifications Attribute Value Input voltage 6-15Vdc 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
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)
KSGYR106F Series Gyro Sensor for Inertial Navigation -45°C to +70°C
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 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
KSGYR104F Fibre Optic Gyroscope ±500°/s 70×70×32mm
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
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
KsINS-02 UAV Inertial Vision Navigation System 1km-8km Range
KsINS-02 Airborne Inertial Vision Navigation System for UAVs Key Specifications Action range 1km~8km Navigation accuracy 1.0m(1σ,lateral accuracy)/20m+1%H (1σ, horizontal positioning accuracy, H is the height of the aircraft relative to the ground) Operating temperature -40℃ ~+60℃ Product Overview The KsINS-02 is an advanced airborne inertial visual navigation system composed of inertial navigation, visible light camera, infrared camera, and AI data processing circuitry.