Series of FOG adopts digital closed-loop and bias mixing technology, all solid-state inertial sensor integrating optics, mechanics and electronics.
Hwa-mins200 is a MEMS inertial navigation system specially developed for short-range missile borne applications.
HWA-BGI2000 airborne FOG integrated navigation system adopts high-precision closed-loop FOG and accelerometer to integrate navigation information with satellite positioning and orientation information, so as to meet the requirements for precise measurement of attitude, heading and position information in the application fields of large UAV and high-precision mobile measurement system.
HWA-BGI2000 has high reliability, stable performance and strong environmental adaptability. The external interface is standard aviation connector, which can be extended and customized according to the user's requirements.