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Single Axis Fiber Optic Gyroscope 9.8*9.8*3cm RS422 Fiber Optic Inertial Navigation System

Wuhan Liocrebif Technology Co., Ltd
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    Buy cheap Single Axis Fiber Optic Gyroscope 9.8*9.8*3cm RS422 Fiber Optic Inertial Navigation System from wholesalers
     
    Buy cheap Single Axis Fiber Optic Gyroscope 9.8*9.8*3cm RS422 Fiber Optic Inertial Navigation System from wholesalers
    • Buy cheap Single Axis Fiber Optic Gyroscope 9.8*9.8*3cm RS422 Fiber Optic Inertial Navigation System from wholesalers
    • Buy cheap Single Axis Fiber Optic Gyroscope 9.8*9.8*3cm RS422 Fiber Optic Inertial Navigation System from wholesalers

    Single Axis Fiber Optic Gyroscope 9.8*9.8*3cm RS422 Fiber Optic Inertial Navigation System

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    Brand Name : Liocrebif
    Model Number : LKF-FS98
    Certification : GJB 9001C-2017
    Price : 5000-25000CHY
    Delivery Time : 2-4 weeks
    Payment Terms : T/T
    Supply Ability : 10000
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    Single Axis Fiber Optic Gyroscope 9.8*9.8*3cm RS422 Fiber Optic Inertial Navigation System

    Essential details
    MOQ:1
    Size:L(9.8)*W(9.8)*H(3.5) cm
    Specification Number:LKF-FS98H
    Introduction

    LKF-FS98H is an inertial angular rate sensor based on the optical Sagnac effect, which is used to measure the angular rate of the carrier along the sensitive axis of the product. The angular rate sensing unit of this product is an optical fiber coil, and a digital closed-loop detection circuit is used to extract the optical path difference of the optical fiber coil sensitive to the clockwise and counterclockwise propagation light caused by the external physical angular velocity, and at the same time, the optical path difference signal is converted into a voltage signal. Closed-loop feedback and control realize signal modulation and demodulation, and achieve the purpose of high-precision angular velocity signal detection.

    By reducing the outer diameter of fiber to 135μm,Thin PM fiber solution decreases extremely the size of fiber coils and delivers outstanding precision performance in fiber coils, which is applied for miniaturization of FOGs. And, the coils are wound precisely through quadrupole symmetry method.The miniatured fiber optic gyros have excellent advantages of compact and cost-effective, and are easy to integrate and ideal for UAV, photoelectric pod, optical platform, and so on.


    Table 1 Performance Parameters Of LKF-FS98H Single-Axis FOG

    A(1310)

    B(1550)

    C(1550)

    D(1550)

    Bias Stability °/hr(1σ,10s)

    ≤0.015

    ≤0.015

    ≤0.010

    ≤0.008

    Time of Stability s

    10

    10

    10

    10

    Bias Repeatability °/hr(1σ)

    ≤0.015

    ≤0.015

    ≤0.010

    ≤0.008

    Bias Repeatability at Full Temperature °/hr

    ≤0.05

    ≤0.05

    ≤0.03

    ≤0.03

    Random Walk Coefficient °/ Single Axis Fiber Optic Gyroscope 9.8*9.8*3cm RS422 Fiber Optic Inertial Navigation System

    ≤0.002

    ≤0.001

    ≤0.001

    ≤0.001

    Scale Factor Non-linearity ppm

    ≤10

    ≤10

    ≤10

    ≤10

    Scale Factor Repeatability ppm

    ≤20

    ≤10

    ≤10

    ≤10

    Scale Factor Repeatability at Full Temperature ppm

    ≤200

    ≤50

    ≤50

    ≤50

    Dynamic Range

    ±500°/s

    Magnetic Susceptibility

    ≤0.020°/hr/Gs

    Working Temperature

    -40+65

    Storage Temperature

    -50+70


    Table 2 The Electrical Interface Of The Gyroscope Uses J30-15ZK Connector

    Pin

    Pin Definition

    Sign

    Color

    1

    Serial port T+

    TX+

    Yellow

    2

    Serial port T-

    TX-

    Orange

    3

    Serial port R+

    RX+

    Blue

    4

    Serial port R-

    RX-

    Green

    5,13

    Power supply+5V

    +5V

    Red

    6,7

    Power ground

    GND

    Black


    Main Features

    High Degree of Engineering, Highly Cost-Effective

    Pure Solid-State Design with Strong Environmental Adaptability

    Long Life and High Reliability, MTBF 20000h

    Single Power Supply (+ 5V), Simplify System Design

    Full Digital RS-422 Electrical Interface Output


    Application

    Photoelectric Pod / Flight Control Platform

    Inertial Measurement Unit

    Surveying and Mapping, Track Inertial Navigation Line Detection

    Platform Stabilization Device, Mobile Communication


    Fig. 1 Dimensions of the external structure


    Single Axis Fiber Optic Gyroscope 9.8*9.8*3cm RS422 Fiber Optic Inertial Navigation System
    Single Axis Fiber Optic Gyroscope 9.8*9.8*3cm RS422 Fiber Optic Inertial Navigation System

    Quality Single Axis Fiber Optic Gyroscope 9.8*9.8*3cm RS422 Fiber Optic Inertial Navigation System for sale
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