TLH-INS-350M-03J Series Fiber Optic Gyro Strapdown Inertial Navigation System

Airborne Strapdown Inertial Navigation System

The TLH-INS-J airborne inertial navigation system integrates a self-developed three-axis fiber optic gyroscope and a three-axis accelerometer (quartz/MEMS). It can be configured to receive external auxiliary positioning information or connect to an external GNSS receiver and other multi-sensors for integrated navigation, effectively meeting the requirements of long-duration, high-precision, and high-reliability navigation applications. The TLH-INS-J series can be widely applied to various types of transport aircraft, unmanned aerial vehicles (UAVs), and other flight control platforms.

· Built-in power-on self-test and anomaly self-diagnosis functions · Supports multiple alignment modes including self-alignment and transfer alignment · Can fuse data from multiple sensors such as pitot tubes, magnetometers, and altimeters · Output protocols, interface definitions, and dimensions can be customized as required · Real-time output of vehicle position, velocity, heading, attitude, and other information · Applicable to electro-optical pods, various low-orbit satellites, various UAVs, various underwater robots, and various unmanned surface vehicles