High Precision FOG INS

High Precision FOG INS

ER-FINS-120 (0.02°):
1. Heading accuracy (1σ): ≤0.02°;
2. Attitude accuracy (1σ): ≤0.02°;
3. Positional accuracy (1σ): 1.0nm/2h.

High Precision FOG INS

High Precision FOG INS

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Introduction

High Precision & High Performance FOG INS 

Introduction 

ER-FINS-120 High Precision & High Performance FOG INS are all strap-down inertial navigation products. The basic components of the series of inertial navigation products are three optical fiber gyroscopes of corresponding grade, three quartz flexible pendulous accelerometer, navigation computer circuit, information processing circuit, current frequency conversion circuit, power changing device, structural platform/structural box and vibration damping device. The product can be used for real-time measurement of three translational information and three moving information of various aircraft or moving objects, and can output real-time navigation information such as angular increment, apparent velocity increment, attitude, speed and position of the carrier. This series of products have the characteristics of wide dynamic working range, strong adaptability to the environment and comprehensive navigation information.

Specifications

Product profile numberER-FINS-120
Boundary dimension200×200×180 mm
Installation dimensions4-Φ8, Installation of central
Weight≤10.0Kg
Power supply18V~36V
Power consumption≤150W
Start time≤1s
Steady working hours≤5min
Alignment time≤5min
Find north precision (1σ)≤0.02°
Speed accuracy (1σ)≤0.05m/s
Attitude accuracy (1σ)≤0.02°
Positional accuracy (1σ)1.0nm/2h
Acceleration measurement range-30g~+30g
Angular velocity measurement range-300°/s~+300°/s
Working temperature-45℃~+65℃
Vibration environment6.6Grms, 5Hz~2000Hz
Shock environment120g, 4ms (1/2sin)
MTBF≥100000h
Working life20years

Application Techniques

1.Inertial Navigation System (INS)

2.What is Inertial Navigation System?

3.MEMS and FOG: How Should you Choose Inertial Navigation System?

4.In Autonomous Flight: How Inertial Navigation Systems Work

5.Development and Application of Inertial Navigation System

6.Introduction to Inertial Navigation Systems


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