TLH-INS-370D-26J-TLH-INS-J Airborne Strapdown Inertial Navigation System-I-NAV - lead the intelligent world with the ultimate high-precision positioning

TLH-INS-370D-26J 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

With the function of secondary calibration, strong autonomy and high reliability, suitability for various complex environments.
Main Functions

With fault self-diagnosis function.
Main Functions

With the functions of receiving external control signals, receiving calibration parameters, re-compensating and outputting gyro and accelerometer information.
Main Functions

With the function of parameter calibration and can accept the writing of calibration parameters.
Main Functions

With the function of real-time output of linear acceleration along three axial directions (X,Y,Z) and angular velocity around the three axes.

Technical features High output frequency, stable and reliable data High circuit integration, navigation solution, plus table IF conversion and other circuit integration design. Integrated design, compact structure, built-in GNSS module and height meter Strong autonomy, autonomous navigation and positioning based on other sensors such as on-board odometers Interface rich, adaptable, with dual CAN, RS422, RS232, synchronous second punch and other types of interface, can be customized according to user needs

Performance Parameters

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