Electronic Gyroscope Sensor
Robust Inertial Navigation System with 160mm X 150mm Installation Dimensions Host ≤ 12.5kg and Spatiotemporal Synchronization Accuracy 0.1m/1ns
Product Description: Essential for any mobile entity is the trio of precision, velocity, and balance. This significance is amplified in the context of sophisticated vehicles such as airplanes, autonomous vehicles, ships, spacecraft, submarines, and unmanned aerial vehicles (UAVs). Here, the necessity for a precise system to manage and govern flawless movement becomes crucial. Inertial navigation systems step in as a vital component, empowering these vehicles to execute their
Inertial navigation system for flight monitoring with accuracy (2σ) Level: 6m, Elevation: 8m
Product Description: Precision, velocity, and balance constitute the foundation for the effective functioning of mobile objects. In the domain of complex vehicles like airplanes, autonomous vehicles, ships, spacecraft, submarines, and unmanned aerial vehicles (UAVs), maintaining an accurate system to regulate and control seamless movement is of utmost importance. Inertial navigation systems emerge as a key solution, enabling these vehicles to perform their tasks with safety
Advanced Inertial Navigation System Aviation with Power Requirement 18V-36V DC
Product Description:The core elements of precision, velocity, and balance are critical for the operation of any moving entity. This holds particularly true for intricate vehicles such as airplanes, autonomous vehicles, ships, spacecraft, submarines, and unmanned aerial vehicles (UAVs), where the necessity for a precise system to manage and control flawless motion is indispensable. Inertial navigation systems play a pivotal role in ensuring that these vehicles can accomplish
High-Performance Inertial Navigation System with Digital input/output RS-422,RS-232 and 100M Ethernet
Product Description: Precision, velocity and balance are key to any moving object. When it comes to complex vehicles, like airplanes, autonomous vehicles, ships, spacecraft, submarines and even unmanned aerial vehicles (UAVs), the need for an accurate system that helps maintain and control perfect movement is essential. With the help of inertial navigation systems, moving vehicles can accomplish their tasks safely and precisely without using GPS. The KsINS-01 integrated
High Precision Low Offset Fiber Optic Gyroscope with ≤0.003°/H Bias Drift for Inertial Navigation Systems
Product Description: This device is an inertial angle rate sensor utilizing the optical Sagnac effect to measure the rotational angular velocity along the sensitive axis of the carrier. A digital closed-loop detection circuit is employed to extract the optical path difference of clockwise light resulting from external physical angular speed. Modulation and demodulation of the optical path signal's voltage enable closed-loop feedback and control, achieving real-time angular
<6W Steady-state Power High precision low offset gyroscope ≤0.001°/H Bias Drift
Product Description: This product functions as an inertial angle rate sensor based on the optical Sagnac effect, measuring the rotational angular velocity along the carrier's sensitive axis. A digital closed-loop detection circuit extracts the optical path difference of clockwise light caused by external physical angular speed. Modulation and demodulation of the optical path signal's voltage enable closed-loop feedback and control, ensuring real-time detection of angular
High Precision Fiber optic gyroscopes for Inertial Navigation Systems (INS) Bias repeatability≤0.001(°/h)
Product Description: This product is an inertial angle rate sensor utilizing the optical Sagnac effect for measuring the rotational angular velocity along the sensitive axis of the carrier. Employing a digital closed-loop detection circuit, it extracts the optical path difference of clockwise light caused by external physical angular speed. Modulation and demodulation of the optical path signal's voltage enable closed-loop feedback and control, achieving real-time angular
High Performance Fiber Optic Gyroscope with ±300°/s Dynamic Range, ≤0.003°/h Bias Drift, and 120×120×38mm Dimensions for Aircraft Attitude Monitoring
Product Description: The Electronic Gyroscope Sensor is a high-performance inclinometer sensor, which is also known as a fiber optic gyroscope or gyro north finder. This cutting-edge technology offers an impressive array of features, including a scale factor non-linearity of ≤5ppm, dimensions of 120×120×38mm, a start time of ≤5s, and a supply voltage of ±5V. It is also able to withstand extreme temperatures, from -50～+80℃. This high-precision gyroscope sensor is ideal for a
High precision and high performance gyroscope for inertial navigation system with Random walk ≤0.0003(º/h^1/2)
Product Description: This device serves as an inertial angle rate sensor, employing the optical Sagnac effect to measure the rotational angular velocity along the carrier's sensitive axis. The digital closed-loop detection circuit is crucial for extracting the optical path difference of clockwise light caused by external physical angular speed. Modulation and demodulation of the optical path signal's voltage enable closed-loop feedback and control, ensuring real-time angular
High precision UAV gyroscope Used in flight control system with Random walk ≤0.0003(º/h^1/2) and Bias drift ≤0.001(°/h)
Product Description: This product, functioning as an inertial angle rate sensor, is based on the optical Sagnac effect for measuring the rotational angular velocity along the carrier's sensitive axis. A digital closed-loop detection circuit is utilized to extract the optical path difference of clockwise light induced by external physical angular speed. Modulation and demodulation of the optical path signal's voltage enable closed-loop feedback and control, achieving real-time
Bias Drift ≤0.1°/H Gyro North Finder with ±5V Supply Voltage for Accurate Navigation and Uav
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 product serves as an inertial angle rate sensor utilizing the optical Sagnac effect for measuring rotational angular
Highly Accurate and ≤0.005º/h^1/2 Low Random Walk Coefficient Electronic Gyroscope Sensor
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. Operating on the principles of the optical Sagnac effect, this device serves as an inertial angle rate sensor, measuring
High precision gyroscopes have a wide range of operating temperatures -40～+70℃ and ±300(°) / S Dynamic range
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. Designed as an inertial angle rate sensor, this product utilizes the optical Sagnac effect for measuring rotational angular
Optical gyroscopes and angular velocity sensors are used in the IMU with ±300(°) / S Dynamic range
Product Description: This device functions as an inertial angle rate sensor utilizing the optical Sagnac effect to measure the rotational angular velocity along the sensitive axis of the carrier. Employing a digital closed-loop detection circuit, it extracts the optical path difference of clockwise light induced by external physical angular speed. The voltage signal from the optical path undergoes modulation and demodulation, enabling closed-loop feedback and control for real
Highly Sensitive Electronic Gyroscope Sensor Dimensions 98×98×35mm
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 demodulation of the optical path signal voltage, closed-loop feedback and control
High precision fiber optical Sagnac effect gyroscope with Random walk coefficient ≤0.005º/h^1/2
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 demodulation of the optical path signal voltage, closed-loop feedback and control
High-performance motion tracking with Electronic Gyroscope Sensor with ≤0.005º/h^1/2 Random walk coefficient
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 demodulation of the optical path signal voltage, closed-loop feedback and control
Fiber Optic Gyroscope with ±500°/s Dynamic Range ≤0.03° Bias Repeatability and ≤10ppm Scale Factor Non-linearity for Angular Velocity Detection
Product Description: This device functions as an inertial angle rate sensor, employing the optical Sagnac effect to measure the rotational angular velocity of the carrier along its sensitive axis. It utilizes a digital closed-loop detection circuit to extract the optical path difference resulting from external physical angular speed in the clockwise direction. Modulation and demodulation of the voltage signal from the optical path enable closed-loop feedback and control,
Fiber optic gyroscope and angular velocity sensor with dynamic range ±900°/s, random walk ≤0.01°/h^1/2, and bias drift ≤0.3°/h for inertial systems
Product Description: This device serves as an inertial angle rate sensor utilizing the optical Sagnac effect to measure the rotational angular velocity of the carrier along its sensitive axis. Employing a digital closed-loop detection circuit, it extracts the optical path difference caused by external physical angular speed in a clockwise direction. Through modulation and demodulation of the optical path signal voltage, closed-loop feedback and control are implemented,
High precision gyroscope detects angular velocity in real time with weight ＜130g and Dimensions
High precision gyroscope detects angular velocity in real time Product Description Operating on the optical Sagnac effect, this product functions as an inertial angle rate sensor designed to measure the rotational angular velocity of the carrier along its sensitive axis. A digital closed-loop detection circuit is utilized to capture the optical path difference induced by external physical angular speed in a clockwise direction. The voltage signal of the optical path is