I6700 SERIES is MEMS integrated navigation system uses high-precision gyroscopes, accelerometers, magnetic sensors, temperature sensors, barometers, satellite receivers, and other sensors, which can replace advanced products with similar performance in Europe and America, as well as fiber optic integrated navigation products with equivalent accuracy. Customized services can be provided according to user needs. At the same time, it can receive satellite differential system reference station information and use high-performance navigation algorithms to fuse multi-sensor information. It can output high-precision navigation information such as pitch, roll, heading, speed, position, etc. of the carrier, suitable for vehicles, aircraft, robots, surface vehicles and other carriers. In the most challenging environment, it can provide very superior attitude and navigation data.

I3700 is an integrated navigation system (GNSS/INS) composed of high-performance MEMS sensors, high-precision GNSS systems and high-performance microprocessors.  The built-in self-developed high-reliability integrated navigation algorithm can output the speed, position, attitude and other information of the measured carrier in real time. Users can also externally connect RTCM differential correction data to achieve high-precision RTK positioning. The IP68 waterproof shell-type package can be easily integrated into the user's system. Product model information is as follows:

I3500 is an integrated navigation system (GNSS/INS) composed of high-performance MEMS sensors, high-precision GNSS systems and high-performance microprocessors.  The built-in self-developed high-reliability integrated navigation algorithm can output the speed, position, attitude and other information of the measured carrier in real time. Users can also externally connect RTCM differential correction data to achieve high-precision RTK positioning. The IP68 waterproof shell-type package can be easily integrated into the user's system. Product model information is as follows:

UF300 series is the most cost-effective fiber optic inertial measurement unit with medium to high precision, which can be used for navigation, control, and dynamic measurement. The system adopts a highly reliable three-axis integrated closed-loop fiber optic gyroscope, with comprehensive performance exceeding the imported KVH1750. It can be post processed and replace the imported POS MV. The gyroscope has a high zero bias repeatability of one order of magnitude. You can choose to support one or more firmware such as IE post-processing, external GPS, odometer, multibeam, Doppler depth sounder (DVL), etc.

UF100A fiber optic inertial group is a middle precision and small size IMU as Figure 1 shown. It is used to detect the angular velocity and linear acceleration of the carrier's motion, providing information for the carrier's attitude and navigation control. It has the advantages of small size, light weight, no moving parts, high reliability, and long service life. It can be widely used in aviation, aerospace, ships, weapons, coal mine measurement, automotive electronics and other fields.

Fiber optic gyroscope, as a new type of all solid state gyroscope, has the advantages of fast start-up, wide measurement range, and high reliability. Among them, the U-F3X100 fiber optic gyroscope IMU (inertial measurement unit) is designed for the needs of medium and low precision application backgrounds, using three-axis shared technology, with low cost and stable performance; Structurally, it adopts integrated packaging of light path and circuit, with a simple structure and convenient installation. It can be applied to navigation guidance, attitude measurement and control systems of small missiles and guided bombs.

Fiber optic gyroscope, as a new type of all solid state gyroscope, has the advantages of fast start-up, wide measurement range, and high reliability. Among them, the U-F3X90 fiber optic gyroscope IMU (inertial measurement unit) is designed for the needs of medium and low precision application backgrounds, using three-axis shared technology, with low cost and stable performance; Structurally, it adopts integrated packaging of light path and circuit, with a simple structure and convenient installation. It can be applied to navigation guidance, attitude measurement and control systems of small missiles and guided bombs.

Fiber optical IMU (inertial measurement unit) is a small missile, guided bomb navigation guidance, attitude measurement and control system development of inertial products, by three solid state fiber gyroscope, three quartz accelerometer and data packing board, measuring the carrier movement angular velocity and line acceleration, for the carrier attitude and navigation control, measurement results through the RS422 serial port output.

U7000 series high-precision MEMS-IMU is a highly reliable and cost-effective six axis MEMS inertial sensor combination, which can be widely used in navigation, control, and measurement fields represented by inertial navigation and attitude stability. This series of MEMS inertial measurement units can be configured with different software and hardware according to user needs. For some inertial navigation applications, gyroscopes can be replaced with high-precision or high dynamic MEMS gyroscopes to meet the needs of different users to the greatest extent possible

U5000-IMU sensor is a highly reliable and cost-effective six axis MEMS inertial heading and attitude system, which can be widely used in navigation, control, and measurement fields represented by vehicles, ships, and drones. High performance MEMS gyroscopes and MEMS accelerometers are integrated into the independent structure, and the gyroscopes and accelerometers selected in the system represent the leading level of MEMS process inertial devices. The product can replace STIM-300 IMU, and its core indicators such as full temperature drift, scale factor error, and vibration performance are 3-5 times higher than STIM-300 sensor.

U3500 series is an IMU/VRU/AHRS sensor composed of high-performance MEMS-IMU, magnetometer, and enhanced single axis gyroscope. It is equipped with self-developed adaptive extended Kalman filter, IMU noise dynamic analysis algorithm, and carrier motion state analysis algorithm, which can meet the accuracy of attitude angle under high dynamic conditions and reduce heading angle drift.

The U300-B sensor, launched by Micro-Magic Inc Hi-Tech Company, is a sturdy and durable industrial-grade small-size inertial measurement unit (IMU) that can measure the acceleration, angular velocity and attitude angle (pitch angle, roll angle) parameters of the moving carrier. The U300-B is great replacement of ADIS16460, which uses high-reliability MEMS accelerometers and gyroscopes, and applies a 6-state extended Kalman filter algorithm with appropriate gain to ensure measurement accuracy, and greatly eliminates the problem through various compensations such as nonlinear compensation, orthogonal compensation, temperature compensation and drift compensation. It eliminates error sources and is especially suitable for inertial measurement under motion or vibration conditions to meet strict environmental requirements.