TLH-INS-370D-26J

TLH-INS-370D-26J Fiber Optic Gyro Strapdown Inertial Navigation System TLH-INS-J Airborne Strapdown Inertial Navigation System TLH-INS-J Airborne Inertial Navigation System is equipped with a self-developed three-axis fiber optic gyroscope and three-axis accelerometer (quartz/MEMS), which can be configured to receive external auxiliary positioning information or external GNSS receivers and other multiple sensors to achieve integrated navigation. It can well meet the requirements of long-term, high-precision, and high reliability navigation applications. The TLH-INS-J series can be widely used in various types of transport aircraft, unmanned aerial vehicles, and other flight control platforms. View Performance Parameters

Main Functions

Equipped with power on self-test and abnormal self check functions.
Main Functions

Can integrate multiple sensors such as airspeed tube, magnetometer, altimeter, etc.
Main Functions

Support multiple alignment modes such as self alignment and transfer alignment.
Main Functions

Real time output of carrier position, speed, heading, attitude and other information.

Advantages Capable of multiple serial communication methods. Pre-delivery full-temperature calibration, compensation and adjustment. High sampling frequency, high bandwidth, and strong dynamic adaptability. The output protocol, interface definition, and appearance can be customized according to the requirements.

Performance Parameters

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