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CN

Product

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 an inertial navigation system based on domestic high-precision optical fiber and quartz flexible accelerometer/MEMS accelerometer. It can be combined with GNSS, altimeter, airspeed indicator and other auxiliary equipment to provide navigation information such as speed, position and attitude for air carriers.
TLH-INS-J Airborne Inertial Navigation System 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 real-time output of information such as carrier position, heading, attitude angle, angular rate and speed

  • Main Functions

    Supporting working modes of pure inertial navigation, INS/GNSS (including Beidou) integrated navigation, etc.

  • Main Functions

    With the function of receiving satellite navigation information provided by external time and frequency standard equipment

  • Main Functions

    With ground self-alignment function and air alignment function

  • Main Functions

    With functions of power-on self-test and periodic self-test

  • Main Functions

    With functions of status reporting, installation error compensation, etc.

Advantages

High sampling frequency, high bandwidth and strong dynamic adaptability

Adopting unique full temperature compensation and calibration technology

Beidou/GPS, altimeter and airspeed indicator integrated functions

Supporting communication modes of RS422, RS232 and CAN digital communication

Customizable output protocol, interface definition and appearance according to requirements

Performance Parameters

  • For more details, please contact us.

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