Found 48 Results For "

optical gyroscope

High Accuracy Single Axis Fiber Optic Gyroscope with 0.002 °/hr Bias Drift and ±300 °/s Angular Rate

F120HC High Accuracy Single-Axis Fiber Optic Gyroscope Model F120HC High Accuracy Single-axis Fiber Optic Gyroscope with 0.002/hr Bias Drift Product Introduction Working Principle and Function This product is an inertial angular rate sensor based on the Sagnac effect principle, designed to measure angular rate movement of the carrier around the sensor's sensitive axis. The unit utilizes a fiber optic coil as the angular rate sensitive unit with closed-loop detection

Compact And Lightweight TDF42IMU0 Fiber Optic Inertial Unit with Low Power Consumption and High Accuracy

TDF42IMU0 Fiber Optic Inertial Unit The TDF42IMU0 fiber optic inertial unit offers compact size, lightweight construction, low power consumption, and high precision performance. Designed for demanding applications with significant impact and vibration, this unit is ideal for small, high-precision inertial measurement in torpedo systems, land/airborne weapons, missile platforms, and other dynamic motion measurement scenarios. Key Features Compact dimensions: 115 * 94 * 50 mm (

Model FG-300AH Cost-effective Military Standard Attitude And Heading Reference System with Fiber-optic Gyroscope

Model FG-300AH Attitude And Heading Reference System The FG-300AH Attitude and Heading Reference System (AHRS) is a cost-effective inertial navigation and measurement solution designed to measure three-dimensional attitude, angular velocity, acceleration, and other motion parameters of carriers. Manufactured according to military standards, this system delivers reliable performance in demanding environments. System Overview The FG-300AH utilizes fiber-optic gyroscope

TDF645B Airborne Optical Gyro Inertial Navigation System with ≤20μg Bias Repeatability, ＞15000 hours MTBF, and Multi-sensor Fusion

Aviation Navigation TDF645B Airborne Optical Gyro Inertial Navigation The Airborne Optical Gyro Inertial Navigation System (INS) employs optical gyroscopes and quartz accelerometers as its core sensing components, utilizing either a strapdown or dithered (modulated) system architecture. Operating with advanced navigation software at high processing speeds, the system delivers real-time navigation data through its sophisticated computational core. This product series features

Quality TDL46A Vehicle Mounted Optical Gyro Positioning Equipment with ≤0.3%D Position Accuracy ≤8min Alignment Time and High Reliability Inertial Navigation System factory

TDL46A Vehicle Mounted Optical Gyro Positioning Equipment with ≤0.3%D Position Accuracy ≤8min Alignment Time and High Reliability Inertial Navigation System

Land Force Navigation TDL46A Optical Gyro Positioning Orientation Equipment Vehicle Mounted The TDL46A vehicle-mounted optical gyro positioning and orientation system employs advanced laser or fiber optic gyroscopes combined with quartz accelerometers as core inertial sensors. Utilizing a strapdown inertial navigation system (SINS) architecture with sophisticated navigation algorithms, it delivers real-time positioning, orientation, and navigation data for diverse vehicular

Quality Land Force Navigation TDL85A Vehicle Mounted Optical Gyro Positioning Equipment with ≤0.003°/h Bias Repeatability, ≥±400°/sec Angular Rate, and ＜8kg Weight factory

Land Force Navigation TDL85A Vehicle Mounted Optical Gyro Positioning Equipment with ≤0.003°/h Bias Repeatability, ≥±400°/sec Angular Rate, and ＜8kg Weight

Land Force Navigation TDL85A Vehicle Mounted Optical Gyro Positioning Orientation Equipment This vehicle-mounted optical gyro positioning and orientation system utilizes laser or fiber optic gyroscopes combined with quartz accelerometers as its core sensors. Employing a strapdown inertial navigation system (SINS) architecture with advanced navigation software, it delivers real-time navigation data through multiple operational modes. System Capabilities The equipment provides

TDF71A Airborne Optical Gyro Inertial Navigation System with ≤20μg Bias Repeatability, ＞20000 hours MTBF, and ≤0.005°/√hr Random Walk

Aviation Navigation TDF71A Airborne Optical Gyro Inertial Navigation The TDF71A airborne optical gyro inertial navigation system employs optical gyroscopes and quartz accelerometers as core sensing components, utilizing strapdown or modulated system architecture. With high-speed embedded navigation algorithms, it delivers real-time positioning and orientation data. This system integrates satellite-based (GNSS), celestial, barometric altimeter, radio navigation, and visual

Quality Aviation Navigation TDF46A Airborne Optical Gyro Inertial Navigation System with ≤0.008°/hr Bias Repeatability, ＞20000 hours MTBF, and ≤20μg Months Bias Repeatability factory

Aviation Navigation TDF46A Airborne Optical Gyro Inertial Navigation System with ≤0.008°/hr Bias Repeatability, ＞20000 hours MTBF, and ≤20μg Months Bias Repeatability

Aviation Navigation TDF46A Airborne Optical Gyro Inertial Navigation The TDF46A airborne optical gyro inertial navigation system employs fiber-optic gyroscopes (FOGs) and high-precision quartz accelerometers as core sensing elements. Operating under strapdown or modulated system architectures, it utilizes advanced navigation algorithms processed through embedded computing units to achieve real-time inertial parameter calculation at refresh rates exceeding 200Hz. Multi-Sensor

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Inertial Navigation System

Fiber Optic Gyrocompass

Fiber Optic Gyroscope

Marine ARPA Radar

Single Beam Echo Sounder

Multi Beam Echo Sounder

Side Scan Sonnar

Underwater Positioning System

Gyrcompass Testing Turntable

Reconditioned Gyrosphere

Global Maritime Distress And Safety System

Electronic Chart Display And Information System

Speed Log

Thermal Imaging Camera System

Inertial Measurement Unit