SNC500A

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SNC500A
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SNC500A fiber integrated navigation system is based on high-precision closed-loop fiber optic gyroscope, accelerometer and high-end GNSS receiving board, through multi-sensor fusion and rotation modulation navigation solution algorithm, to provide high-precision attitude, speed and position, to meet the requirements of high-precision measurement and control. 


 Physical Dimensions and Electrical Index

 Voltage

 24-36V

 Power Consumption

≤30W

 Size

 199mm×180mm×219.5mm

 Weight

≤7.5kg(Non-aircraft Type)

≤6.5kg(Aircraft Type)

 Environmental Index

 Working Temperature

-40℃~+60℃

 Storage Temperature

-45℃~+70℃

 Vibration

 5~2000Hz6.06g(With Shock Absorption)

 Shock

 30g11ms(With Shock Absorption)

 Lifetime

>15 years

 Continuous Working Time

>24h

 Interface Features

 RS422×7

 RS232×2

 PPS×1

 System Performance Index                                        


 Test Conditions

 Index

 Position Accuracy

 GNSS Valid,Single point

1.2m(RMS)

 GNSS Valid,RTK

 2cm+1ppm(RMS)

 Position Maintenance(GNSS Invalid)

 0.8nm/h(CEP), 3.0nm/3h(CEP)

 1‰D(D is for distance

 Heading Accuracy

 North Seeking

 0.06°×sec(Lati)

 0.03°×sec(Lati)

 Heading Maintenance(GNSS Invalid)

 0.02°/h(RMS), 0.05°/3h(RMS)

 Attitude Accuracy

 GNSS Valid

 0.01°(RMS)

 Attitude Maintenance(GNSS Invalid)

 0.01°/h(RMS), 0.03°/3h(RMS)

 Speed Accuracy

 GNSS ValidSingle Point L1/L2

 0.1m/s(RMS)

 Speed MaintenanceGNSS Invalid

 0.8m/s/h(RMS), 3m/s/3h(RMS)

 IMU Performance Index

 FOG

 Operating Range

±400°/s

 Bias Stability

≤0.01°/h

Quartz Flexible Accelerometer

 Operating Range

±20g

 Bias Stability

≤20μg


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