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Single Axis Interferometric Fiber Optic Gyroscope Compact For Navigation

Wuhan Liocrebif Technology Co., Ltd
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Single Axis Interferometric Fiber Optic Gyroscope Compact For Navigation

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Brand Name : Liocrebif

Model Number : LKF-FS50X

Place of Origin : China

Certification : GJB 9001C-2017

Price : 5000-25000CHY

MOQ : 1

Packaging Details : Wooden box/Cardboard box/Container

Delivery Time : 2-4 weeks

Payment Terms : T/T

Supply Ability : 10000

Color&Classification : LKF-FS50X

Dimensions : 52*52*39mm

Bandwidth : 1000Hz

Brand : LIOCREBIF

Application : UAVs, mobile communication systems, fiber optic pods, platform stabilization devices

Electricity : RS422

Original Place : China

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Essential details
MOQ:1
Size:L(5)*W(5)*H(3.65) cm
Specification Number:LKF-FS50X
Product Introduction

Introduction

LKF-FS50X is a miniaturized closed-loop fiber optic gyroscope, which breaks through the classical design concept of traditional fiber optic gyroscope. It adopts integrated circuit and optical path design. It has the outstanding characteristics of small volume, light weight, high bandwidth, fast start-up, simple interface and convenient use. LKF-FS50X is an ideal medium-low precision angular rate sensor in the control field, which is widely used in various inertial measurement and control fields.

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.

By using inertial devices and strapdown inertial navigation technology, accurate speed, position and attitude information can be provided for the UAV, thereby achieving precise navigation, positioning and attitude control. LKF-FS50X can greatly improve the performance of inertial navigation and is an ideal choice for medium-low precision inertial navigation.

Table 1 Performance parameters of LKF-FS50A single-axis FOG

A

B

C

Bias Stability °/hr(1σ,10s)

≤0.30

≤0.20

≤0.10

Stabilization Time S

<10

<10

<10

Bias Repeatability °/hr(1σ)

≤0.30

≤0.20

≤0.10

Full Temperature Bias Repeatability °/hr

≤1

≤0.5

≤0.3

Random Walk Coefficient °/Single Axis Interferometric Fiber Optic Gyroscope Compact For Navigation

≤0.02

≤0.02

≤0.01

Scale Factor Nonlinearity ppm(1σ)

≤100

≤50

≤50

Scale Factor Repeatability ppm(1σ)

≤100

≤50

≤50

Dynamic Range

±500°/s

Magnetic Field Sensitivity

≤0.10°/hr/Gs

Operating Temperature

-40+70

Storage Temperature

-50+70

Vibration Condition

4.2g,20Hz2000Hz

Table 2 Performance parameters of LKF-FS50X single-axis FOG

A

B

C

Bias Stability °/hr(1σ,10s)

≤0.20

≤0.10

≤0.05

Stabilization Time S

<10

<10

<10

Bias Repeatability °/hr(1σ)

≤0.30

≤0.20

≤0.10

Full Temperature Bias Repeatability °/hr

≤0.6

≤0.4

≤0.3

Random Walk Coefficient °/Single Axis Interferometric Fiber Optic Gyroscope Compact For Navigation

≤0.02

≤0.02

≤0.01

Scale Factor Nonlinearity ppm(1σ)

≤50

≤30

≤20

Scale Factor Repeatability ppm(1σ)

≤50

≤30

≤30

Dynamic Range

±500°/s

Magnetic Field Sensitivity

≤0.05°/hr/Gs

Operating Temperature

-40+70

Storage Temperature

-50+70

Vibration Condition

4.2g,20Hz2000Hz

Main Features

Miniature and compact design

Pure solid shell design

Environment Edaptive

High Reliability and Long Life

Fully Digital RS-422 Electrical Output

Application

Electro-optical Pod

Flight Control Platform

Optical/Photographic Platform

Platform Stabilizer

Satcom on the Move

Inertial Measurement Unit

Light UAV

Fig. 1 Dimensions of the external structure FS50A

Single Axis Interferometric Fiber Optic Gyroscope Compact For Navigation

Fig. 2 Dimensions of the external structure FS50X

Single Axis Interferometric Fiber Optic Gyroscope Compact For Navigation
Single Axis Interferometric Fiber Optic Gyroscope Compact For Navigation


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Single Axis Interferometric Fiber Optic Gyroscope

      

Single Axis Gyroscope In Navigation

      

Compact Interferometric Fiber Optic Gyroscope

      
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