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FG-980S Inertial Navigation System

FG-980S Inertial Navigation System, in which the GNSS receiver embedded, adopts three high accuracy single-axis closed-loop miniature FOGs and quartz accelerometers. This system is compact design with very high performance as well as small size, light weight and low power consumption, which is perfectly applicable for UAV, helicopter and aircraft.

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Introduction

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Overview

FG-980S Inertial Navigation System, in which the GNSS receiver embedded, adopts three high accuracy single-axis closed-loop miniature FOGs and quartz accelerometers. This system is compact design with very high performance as well as small size, light weight and low power consumption, which is perfectly applicable for UAV, helicopter and aircraft.

 

Features

•  Provide self-contained, abundant, continuous and accurate navigation information

•  Small size, light weight and low power consumption

•  Embedded satellite navigation technology

Applications

UAVS , Helicopter , General Aviation Aircraft ,  etc.

 

Structural Dimension

 

Specifications

Alignment Time GC:10min
Fast:5min
Accuracy Position Inertial:1nm/h
Integrated:20m
Velocity Inertial:1m/s
Integrated:0.8m/s
 
Attitude Inertial:0.02°
Integrated:0.01°
Heading Inertial:0.1°
Integrated:0.08°
Dynamic Range Angular Rate ±400°/s
Acceleration ±15g
Operation Requirement Temperature Operating:-45~+70℃
Storage:-55~+85℃
Shock Half-sinusoid:15g,11ms
Vibration 0.04g2/Hz
MTBF 50000h
Power Supply/Consumption 28VDC/30W
Interface MIL-STD-1553B
ARINC-429
RS-422
Dimension Navigation unit:238mm×188mm×190mm
Max size:254mm×188mm×190mm
Weight 7.1kg(excluding receiving antenna)

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