FOG-based INS

BTSTC-INS0140

BTSTC-INS0140 inertial navigation system uses fiber optic gyroscope and quartz flexible accelerometer as inertial sensing devices, and integrates navigation computer, I/F conversion, DC power supply, satellite receiver and other supporting circuits.

View more

BTSTC-0470S

BTSTC-70S integrated navigation system is based on three-axis high-precision fiber optic gyroscope, quartz flexible accelerometer and high-precision satellite positioning device.

View more

BTSTC-0440S

BTSTC-40S integrated navigation system is based on three-axis fiber optic gyroscope, quartz flexible accelerometer and high-precision satellite positioning device.

View more
< 1 >