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CN

Product

TLH-INS-350D-23J

Fiber Optic Gyro Strapdown Inertial Navigation System
TLH-INS-J Airborne Strapdown Inertial Navigation System

Hybrid Inertial Measurement Unit is composed of MEMS IMU and single-axis 60 fiber optic gyro. Since the vehicle pays more attention to heading accuracy, the Z-axis of MEMS is replaced by high-precision fiber optic gyro, which in turn calculates and outputs roll angle, pitch angle and heading angle. It is used to measure the attitude and orientation of various moving objects and is widely used in the field of automatic driving.
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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