INS500 fiber integrated navigation system (the "ins") by the closed loop based on high precision fiber optic gyro, accelerometer and high-end GNSS receiver boards, navigation through multiple sensor fusion and decoding algorithm, provide high precision navigation position, velocity and position information, such as meet the requirement of high precision measurement and control, and main application fields include: The system has inertial/satellite integrated navigation mode and pure inertial mode. When GNSS is invalid, it can enter the pure inertia mode (that is, GPS fusion has never been carried out after power is turned on, if the fusion is lost again, it belongs to the integrated navigation mode). After starting, it has accurate attitude measurement function, can output pitch roll course, and pure inertia can static north search.

GPS navigation sensor high precise inertial sensor with GPS INS500 fiber integrated navigation system (the "ins") by the closed loop based on high precision fiber optic gyro, accelerometer and high-end GNSS receiver boards, navigation through multiple sensor fusion and decoding algorithm, provide high precision navigation position, velocity and position information, such as meet the requirement of high precision measurement and control, and main application fields include: The system has inertial/satellite integrated navigation mode and pure inertial mode. When GNSS is invalid, it can enter the pure inertia mode (that is, GPS fusion has never been carried out after power is turned on, if the fusion is lost again, it belongs to the integrated navigation mode). After starting, it has accurate attitude measurement function, can output pitch roll course, and pure inertia can static north search.

Product features Small size light weight low cost strong environmental adaptability anti-disturbance suitable for harsh use environment High accuracy and large measurement range Field of application Unmanned aerial vehicles, guided bombs, missiles, rockets, platform stabilization. This product adopts highly integrated MEMS gyroscope and accelerometer IMUs GPS-OEM board, barometric altimeter, magnetometer and other multi-purpose sensors, uses Kalman filtering technology to fuse SINS and GPS information, and outputs stable and reliable navigation parameters such as heading, attitude, speed and position. Gyroscopes mainly include MEMS gyroscopes and fiber optic gyroscopes.

6 axis attitude sensor, precise navigation sensor with GPS, inertial navigation GPS sensor Field of application Unmanned aerial vehicles, guided bombs, missiles, rockets, platform stabilization. This product adopts highly integrated MEMS gyroscope and accelerometer IMUs GPS-OEM board, barometric altimeter, magnetometer and other multi-purpose sensors, uses Kalman filtering technology to fuse SINS and GPS information, and outputs stable and reliable navigation parameters such as heading, attitude, speed and position. Gyroscopes mainly include MEMS gyroscopes and fiber optic gyroscopes.

This product adopts highly integrated MEMS gyroscope and accelerometer IMUs GPS-OEM board, barometric altimeter, magnetometer and other multi-purpose sensors, uses Kalman filtering technology to fuse SINS and GPS information, and outputs stable and reliable navigation parameters such as heading, attitude, speed and position. Gyroscopes mainly include MEMS gyroscopes and fiber optic gyroscopes.