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774.3cm Gyro Navigation System Fiber Optic Gyro High Performance For Photoelectric Pod

Name: 7743cm Gyro Navigation System Fiber Optic Gyro High Performance For Photoelectric Pod
Brand: Liocrebif
Price: 5000 USD

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Brand Name :	Liocrebif
Model Number :	LKF-F3G40
Certification :	GJB 9001C-2017
Price :	5000-25000CHY
Payment Terms :	T/T
Supply Ability :	10000
Delivery Time :	2-4 weeks

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Product Details
Company Profile

774.3cm Gyro Navigation System Fiber Optic Gyro High Performance For Photoelectric Pod

Essential details

MOQ:1

Size:L(7)*W(7)*H(4.3) cm

Specification Number:LKF-F3G40

Product Introduction

Introduction

F3G40 3-axis FOG is an inertial product developed for inertial navigation, attitude measurement and control systems of small missiles and guided bombs. The angular velocity and linear acceleration of the carrier motion provide information for the attitude and navigation control of the carrier, and the measurement results are output through the RS422 serial port.

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 three-axis fiber-optic gyroscope can provide high-precision attitude angular velocity data to help the UAV achieve accurate attitude control and navigation. By monitoring the UAV's 3D rotational motion in real time, the gyroscope data can be fused with GPS and other sensor data to ensure the stability and accuracy of the UAV in flight.

Table 1 Performance parameters of LKF-F3G40 Three-axis FOG

No.	Test items	Unit	Requirement
1	Start-up Time	s	3
2	Bias Stability (10s smoothing)	(°)/h	≤0.1
3	Bias Repeatability	(°)/h	≤0.1
4	Random Walk Factor	(º) /h^1/2	≤0.01
5	Scale Factor Nonlinearity	ppm	≤20
6	Scale Factor Repeatability	ppm	≤20
7	Operating Temperature	℃	-45~+70
8	Storage Temperature	℃	-55~+80
9	Dynamic Range	(°)/s	±500
10	Power Supply Voltage	V	+5V
11	power Consumption in Steady State (full temperature)	W	≤8

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

No.	Defination	Notes
1	+5V	Power supply input
2	GND	Power supply ground
3	RETAIN
4	RXD+	Gyro differential select positive
5	TXD+	Gyro RS422 output positive
6	+5V	Power supply input
7	GND	Power supply ground
8	RXD-	Gyro differential select negative
9	TXD-	Gyro RS422 output negative

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

图示, 工程绘图描述已自动生成

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774.3cm Gyro Navigation System Fiber Optic Gyro High Performance For Photoelectric Pod

774.3cm Gyro Navigation System Fiber Optic Gyro High Performance For Photoelectric Pod

774.3cm Gyro Navigation System Fiber Optic Gyro High Performance For Photoelectric Pod

774.3cm Gyro Navigation System

774.3cm Fiber Optic Gyro

High Performance Gyro Navigation System

774.3cm Gyro Navigation System Fiber Optic Gyro High Performance For Photoelectric Pod

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7*7*4.3cm Gyro Navigation System Fiber Optic Gyro High Performance For Photoelectric Pod

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774.3cm Gyro Navigation System Fiber Optic Gyro High Performance For Photoelectric Pod