SNC300G-A0

CURRENT POSITION: HOME > SNC300G-A0

SNC300G-A0
Product type:
Views:
  • Details
  • Specifications

SNC300G-A0 is a compact INS with FOG and MEMS accelerometer. It can use accurate timing and positioning information of external GNSS to carry out inertial/satellite integrated navigation. When external GNSS is invalid, the INS has high precision retention ability of pure inertial navigation.


 Physical Dimensions and Electrical Index

Voltage

11-36V

Power Consumption

≤8W

Size

 111mm×72mm×43mm

Weight

≤500g

 Environmental Index

Working Temperature

-40℃~+60℃

Storage Temperature

-45℃~+70℃

Vibration

 5~2000Hz,6.06g(With Shock Absorption)

Shock

 30g,11ms(With Shock Absorption)

Lifetime

>15 Years

Continuous Working Time

>24h

 Interface Features

 RS422×1

 RS232×2

 PPS×1

 System Performance Index                                    


Test Conditions

Index

 Position Accuracy

External GNSS Valid,Single Point

Superior to External Satellite Position Accuracy

External GNSS Valid,RTK

Superior to External Position Accuracy

Position Maintenance of Pure Inertial Level

300m/6min(CEP)

2nm/20min(CEP)

Airspeed Combination Horizontal Positioning Maintenance

1nm/20min (CEP)

 Heading Accuracy

Single Antenna

0.1°(RMS)(Vehicle Condition,   Maneuvering)

Dual Antenna

0.2°/L(L is Baseline)(RMS)

Heading Maintenance

1°/h(RMS)

Self-North Seeking Accuracy

 1°SecL, Align for 15min(Dual Position Alignment)

 Attitude Accuracy

GNSS Valid

 0.05°(RMS)

Attitude Maintenance(GNSS Invalid)

 1°/h(RMS)

 Speed Accuracy

GNSS Valid, Single Point L1/L2

 No lower than the Positioning Accuracy of External Satellites


联系我们
关闭

微信

客户服务热线

010-83634152

联系我们

在线客服