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FS300-70 Optical Fiber Integrated Navigation System
Fiber optic integrated navigation system FS300-70 is based on cost-effective closed-loop fiber optic gyroscope, accelerometer and high-end GNSS receiving board, and is realized by multi-sensor fusion and navigation solution algorithm. It can meet the requirements for accurate measurement of attitude, heading and position information in medium and high precision mobile measurement systems, large unmanned aerial vehicles and other applications.
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FS300-42 Optical Fiber Integrated Navigation System
The Optical Fiber Integrated Navigation System FS300-42 is comprised of a small and lightweight-axis integrated closed-loop fiber optic gyroscope, accelerometer, and guidance card, all of which are cost-effective. This system utilizes multi-sensor fusion and navigation algorithms to accurately measure attitude, heading, and position information. It is suitable for use in medium to high precision mobile measurement systems and medium to large UAVs.
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M200C-IMU Inertial Measurement Unit
M200C-IMU is a micromechanical technology (MEMS) based inertial measurement unit (IMU) with built-in high performance MEMS gyro and MEMS accelerometer, outputting 3 angular velocities and 3 accelerations.
M200C-IMU has high reliability and environmental adaptability. By matching different software, the product can be widely used in guided munitions, tactical and industrial UAVs, guidance heads, autopilot and other fields.
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MS100-B0 Combined Navigation System
MS100-B0 Combined Navigation System (hereinafter referred to as Combined Navigation System) has built-in high-performance MEMS gyro and accelerometer, which can receive internal GNSS data, realize multi-sensor fusion and combined navigation solution algorithm, and have short-time inertial navigation capability when GNSS is invalid.
The product is highly reliable and highly adaptable to the environment. By matching different software, the product can be widely used in tactical and industrial UAVs, unmanned vehicles, unmanned ships, aerial guided bombs, smart munitions, rockets, kinetic mid-range, mapping, guidance heads and stabilization platforms. -
AS-001 High -Precision Inclination Instrument
AS-001 is a triaxial accelerometer based on micromechanical technology, by measuring the acceleration velocity meter and using advanced signal processing algorithm technology to get high precision inclination information under complex working conditions. The product is benchmarked against the performance of servo inclinometers. The product is benchmarked against the performance of servo inclinometers, with both 4~20mA analog output and digital output in two forms.
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MS-100A0 Attitude Measurement System
MS-100A0 is an advanced three-degree-of-freedom attitude measurement system based on micro-mechanical technology (MEMS). It incorporates a high-performance MEMS gyroscope and MEMS accelerometer, which work in tandem to accurately calculate the pitch angle, roll angle, and heading angle of the carrier in real-time. Additionally, it offers the option to integrate a magnetometer for achieving high-precision north finding. The system provides output data on 3-axis angular velocity and 3-axis acceleration, which can be effectively utilized for motion control purposes.
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Type 120 Single Axis High Precision Gyroscope
Product features
◆ High precision
◆ No moving parts
◆ High reliability and long life
Application scenario
◆ Photoelectric stabilization
◆ Radar control
◆ Missile guidance
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Type 98 Single Axis High Precision Gyroscope
Product features
◆ High precision
◆ No moving parts
◆ High reliability and long life
Application scenario
◆ Photoelectric stabilization
◆ Radar control
◆ Missile guidance
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Type 75 Single Axis Medium Precision Gyroscope
Product features
◆ Small size, light weight, high precision
◆ No moving parts
◆ High reliability and long life
Application scenario
◆ Medium and high precision inertial navigation system
◆ Missile weapon
◆ Underwater weapon
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Type 70 Single Axis Low Precision Gyroscope
Product features
◆ Small size and light weight
◆ No moving parts
◆ High reliability and long life
Application scenario
◆ Photoelectric stabilization
◆ Radar control
◆ Missile guidance
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Type 50 Single Axis Low Precision Gyroscope
Product features
◆ Small size and light weight
◆ No moving parts
◆ High reliability and long life
Application scenario
◆ Photoelectric stabilization
◆ Radar control
◆ Missile guidance
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RLG Two-Axis Indexing Inertial Navigation System
RLG-2HX90 inertial navigation system is an inertial navigation system based on type 90 ring laser gyroscope and quartz flexible accelerometer. It can be combined with auxiliary equipment such as GNSS, altimeter, airspeed meter, etc., and can provide air carrier, ground carrier, etc. Navigation information such as speed, position, and attitude.
The Type 90 series inertial navigation system can be widely used in carrier platforms such as tanks, various types of armored vehicles, self-propelled artillery, rockets, various types of aircraft, drones, ships, automobiles, high-speed rail, unmanned vehicles, mobile satellite communication systems, and drilling. Flight control, attitude stabilization, weapon stabilization platform, positioning and orientation, etc.
