Electronic Gyroscope Sensor
Advanced Visual Inertial Navigation System for Aircraft with AI Data Processing, Navigation Accuracy 1.0m, and Weight ≤2.0kg
Product Description: Designed as an airborne inertial visual navigation system, the KsINS-02 integrates inertial navigation, visible light camera, infrared camera, and an AI data processing circuit. By leveraging the principles of optical imaging and inertial measurement, it provides UAVs with a wealth of information, including inertial/visual combined attitude, speed, position, angular velocity, acceleration, and more. This product incorporates artificial intelligence
High Precision Inertial Navigation Gyro with ≤0.001(°/h) Bias Repeatability and ±300(°/s) Dynamic Range in 120×120×38(mm) Compact Design
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
Precision Electronic Gyroscope Sensor with ≤0.005º/H^1/2 Random Walk Coefficient, ≤10ppm Scale Factor Repeatability, and Compact 98×98×35mm Dimensions for Navigation
Product Description: The Electronic Gyroscope Sensor is a compact and reliable fiber optic gyroscope with high accuracy and stability. It features excellent dynamic range, low power consumption, wide-operating temperature range and low cost. It is a perfect choice for applications involving precision navigation, attitude measurement, and motion control. This device functions as an inertial angle rate sensor utilizing the optical Sagnac effect to measure the rotational angular
±5V Supply Voltage Electronic Gyroscope Sensor with ±300°/s Dynamic Range and ≤0.03°/h Bias Repeatability for Robotics
±5V Supply Voltage Electronic Gyroscope Sensor for Robotics Applications Product Description: This product serves as an inertial angle rate sensor utilizing the optical Sagnac effect for measuring rotational angular velocity along the sensitive axis of the carrier. The incorporation of a digital closed-loop detection circuit facilitates the extraction of the optical path difference induced by external physical angular speed in clockwise light. Through modulation and
High Precision Fiber Optic Gyroscope with 120×120×38 mm Dimensions and -45～+70°C Operate Temperature for Inertial Measurement
KSFG-120series 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
70×70×32 mm Optical Gyroscope with 5s Start Time and -40～+70℃ Operate Temperature for Inertial Navigation Systems
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
High Precision Digital Optical Gyroscope with 70×70×32 mm Dimensions and -40℃～+70℃ Operating Temperature for UAV Navigation
K1FOG40 series 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
Integrated Navigation Processing Equipment for Missile Launch Reference with ≤100W Power, -40℃~+65℃ Range, and Dual Redundant Interfaces
KsINS-A Integrated navigation processing equipment for launch reference Product Description Integrated navigation processing equipment for launch reference is used to provide accurate, continuous and smooth navigation reference information for missile alignment. It can receive multiple sets of inertial navigation equipment data to complete functions such as synchronization, smoothing, redundant monitoring and diagnosis of multiple inertial navigation data information; it can
High Precision Lightweight MEMS Navigation System with Low Power Consumption for Unmanned Vehicles and Drones
KsINS-W72 MEMS inertial/satellite integrated navigation system Product Description KsINS-W72 is a small high-precision MEMS serialized product. It consists of 3 high-precision MEMS gyroscopes, 3 high-precision MEMS accelerometers, a microprocessor, and a satellite receiver. It is suitable for various types of integrated navigation and short-term pure navigation. Inertial navigation, guidance and control application fields. The basic functions of the integrated navigation
Fiber Optic Gyroscope Inertial Navigation System with ≤ 20W Power Consumption, 0.01°/h Bias Stability, and -40℃ to +65℃ Operating Temperature
KsINS-90 type optical fiber strapdown inertial navigation system product description: The KsINS-90 fiber optic gyroscope strapdown navigation system is based on a universal fiber optic inertial navigation platform. The platform adopts a universal design concept and is easy to make adaptive changes according to user needs. It has the advantages of short development cycle, high maturity, and good reliability. ; Its supporting gyroscopes, accelerometers, circuits and other
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
Medium Precision Fiber Optic Strapdown Inertial Navigation System Posture ≤0.05°, 1σ,weight 3.6kg
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,
Medium Precision Fiber Optic Strapdown Inertial Navigation System For Maritime Use, Input Voltage 18V~36V, MTBF ≥30000h
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,
Medium Precision Fiber Optic Strapdown Inertial Navigation, Alignment Time 5min, Service Temperature -40 ° C To +60 °C
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,
Inertial Measurement Unit Automatic Control Mapping Satellite Combination ≤5m CEP DVL Combination ≤1%D CEP
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,
1.6kg Aerospace Inertial Navigation System with Scale Factor Stability ≤100ug 1σ and MTBF ≥30000h
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,
Defense Inertial Navigation System Input Voltage 18V-36V Power Dissipation ≤20W
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,
Precision Electronic Gyroscope Sensor for Harsh Environments with RS422 Interface and 6.06 G Vibration Tolerance
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
Precision Dual Redundancy Gyro Sensor with RS422 Interface and -40~65℃ Operating Temperature
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
Speed 460800bps RS422 Gyroscope Sensor For Precision Navigation，Bias 0±0.02g
Product Description: KQ6IMU100 is a cutting-edge inertial measurement module that has been developed using innovative MEMS technology. One of its key functionalities is the ability to accurately measure angular velocity and acceleration data of the carrier in three dimensions. MEMS is a highly advanced micro-device or system, which incorporates a number of micro-components such as micro-sensors, micro-actuators, micro-mechanical structures, micro-power and micro-energy