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.

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BTSTC-INS04100A

BTSTC-100A integrated navigation system is equipped with high-precision positioning and orientation receiver, high-performance MEMS inertial measurement unit, magnetometer and barometer, which can realize rapid positioning and orientation of dual antennas, and also can maintain position, speed and attitude accuracy for a long time. It can switch between that pure inertial navigation mode and the combined navigation mode accord to the satellite positioning condition.

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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.

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BTSTC-0440S

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

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BTSTC-04200S-F

The BTSTC-200S-F integrated navigation system is equipped with a high-precision satellite navigation device, a high-performance MEMS inertial measurement unit, and a large-capacity data recorder.

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BTSTC-048K22

The BTSTC-8K22 integrated navigation system measures the relevant data of the carrier through the internal high-precision MEMS inertial measurement unit and the high dynamic satellite navigation receiver

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BTSTC-INS0202

The INS02 is a small, lightweight, self-contained and full attitude inertial /GNSS navigator designed for applications that require stable, continuous position and attitude navigation data.

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