• Nine Axis Output Combined Navigation System for Airplane Ship Vehicle Guidance
  • Nine Axis Output Combined Navigation System for Airplane Ship Vehicle Guidance
  • Nine Axis Output Combined Navigation System for Airplane Ship Vehicle Guidance

Nine Axis Output Combined Navigation System for Airplane Ship Vehicle Guidance

Type: Inertial Navigation
Output Signal Type: Digital Output
Measuring Shaft Quantities: Three
Accuracy Grade: 0.06deg
IP Rating: IP67
Certification: CE
Customization:
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  • Overview
  • Product Description
  • Product Parameters
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  • Company Profile
Overview

Basic Info.

Model NO.
INS300C
Customized
Customized
Heading Accuracy
<0.06deg
Attitude Measurement Accuracy
<0.03deg
Speed Accuracy
<0.03m/S
Position Accuracy
<2cm+1ppm Rtk
Operating Temperature
-40~70
Transport Package
Sponge and Box
Specification
178mm*178mm*135mm
Trademark
AVIC
Origin
China
Production Capacity
100/Month

Product Description

Nine Axis Output Combined Navigation System For Airplane Ship Vehicle Guidance
 

Product Description


Product features: precision, gyro precision 0.008 (°)/H ~ 0.02 (°)/H (10s, 1σ); wide measurement range, ± 300 (°) per second, capable of dual antenna orientation, built-in multi-mode satellite navigation system, test reference GJB5418-2005
Typical should be: 1. Various types of and orientation systems, aerial launching turrets, ground-to-ground missile launching turrets, etc. ship main inertial navigation, medium aircraft main inertial navigation 3. Radar position measurement of medium array
 

Product Parameters

 
Technical indicators:


Work performance
Parameter name Unit INS-300C
Satellite navigation signal is valid
North seeking heading accuracy   ≤ 0.1/cosL, (1σ) (L is the local latitude)
Heading Accuracy ° ≤0.06,(1σ)
Attitude measurement accuracy   ≤0.03,(1σ)
Speed accuracy m/s ≤0.03
Position accuracy m ≤2m/RTK2cm(CEP)
Satellite navigation signal failure
Heading  Hold Accuracy   ≤0.06,1h
Attitude holding accuracy   ≤0.03,1h
Pure inertial  position accuracy nmile 0.6(CEP,5h)
System measurement range
Heading Measurement Range   0~360
Attitude Measurement Range   -90~+90
North seeking type Estimate the latitude, shake the base, enter the time (GPS or odometer is valid)
Navigational Pure Inertial, GPS Combination, Range Meter Combination, Meter Combination, Carrier Constraint
1. Environmental parameters
1.1 Make the temperature ºC -40~+70
1.2 Storage temperature ºC -45~+70
1.3 Vibration Hz,g²/Hz 20~2000,0.04
1.4 Impact   20g, 11ms, half sine
2. Electrical parameters
2.1 Power supply Vdc +18~+36
2.2 Power W ≤20
2.3 Data connection / RS-422/CAN
2.4 Data refresh rate Hz ≤ 200 (settable)
3. Physical parameters
3.1 Outline ruler/installation ruler mm ≤178x178x134.5/162x162(4xΦ6.5
3.2 Weight kg ≤4.6

Detailed Photos

Nine Axis Output Combined Navigation System for Airplane Ship Vehicle GuidanceNine Axis Output Combined Navigation System for Airplane Ship Vehicle GuidanceNine Axis Output Combined Navigation System for Airplane Ship Vehicle Guidance


Company Profile


Nine Axis Output Combined Navigation System for Airplane Ship Vehicle GuidanceNine Axis Output Combined Navigation System for Airplane Ship Vehicle Guidance















 

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Gold Member Since 2023

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Trading Company
Number of Employees
7
Year of Establishment
2022-11-23