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Fiber Optic Inertial Navigation System KSINS002C 18-32VDC

Xi'an Kacise Optronics Co.,Ltd.
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Fiber Optic Inertial Navigation System KSINS002C 18-32VDC

Brand Name : KACISE

Model Number : KSINS002C

Certification : CE

Place of Origin : CHINA

MOQ : 1PCS

Supply Ability : 1000 Piece/Pieces per Week negotiable

Delivery Time : 5-8 work days

Packaging Details : each unit has individual box and all boxes are packed in standard packages or customers requests available

Power Voltage : 18~32VDC

Power : <20W

Position Accuracy : <0.05%D;<0.5nmile/h

Attitude Accuracy : <0.02°

Heading accuracy : <0.5mil

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KSINS002C Fiber Optic Strapdown Inertial Navigation System

Product Introduction
The KSINS002C fiber optic gyro strapdown navigation system is based on our institute's fiber optic inertial navigation universal platform. This platform adopts a universal design concept and is easy to make adaptive changes according to user needs. It has a short development cycle, high maturity and good reliability. and other advantages; its supporting gyroscopes, accelerometers, analog-to-digital conversion circuits, navigation computers and other components are all products on our shelves, which are mature and reliable.
Feature
● Using domestic 120 type fiber optic gyroscope and quartz flexible accelerometer
● The bias stability of the 120 type fiber optic gyroscope is better than 0.005°/h (1σ)
● Accelerometer bias stability is better than 50μg (1σ)
● Achieve static and dynamic base alignment, and can choose self-alignment or on-the-fly alignment according to user needs
● It can be integrated with various information such as satellites, laser speedometers, odometers, altimeters, etc. for combined navigation, and the interface has strong scalability
Application
● Land Use
● Marine Navigation
● Unmanned Aerial Vehicles

Fiber Optic Inertial Navigation System KSINS002C 18-32VDC
Technical Specifications

Parameter

KSINS002C

Power supply parameter

Power Voltage

18~32VDC

Power

<20W

Product performance

Navigation

Position Accuracy

<0.05%D;<0.5nmile/h

Attitude Accuracy

<0.02°

Heading accuracy

<0.5mil

Circular Error Probable(CEP)

<0.1m

Velocity Accuracy

<0.8m/s

Alignment Time

<5min

Gyroscope

Bias stability

≤ 0.005°/h

Bias repeatability

≤ 0.005°/h

scale factor temperature sensitivity

30ppm

Random walk

≤ 0.001°/√h

Accelerometer

Bias stability

≤ 100μg

Bias repeatability

≤ 50μg

Scale factor repeatability

50ppm

scale factor temperature sensitivity

50ppm

Environment

Operating temperature

-40~+65°C

Random vibration

GJB150.16A-2009.C.3

shock

30g,11ms

Output

RS-422 × 2;RS-232 × 1;Ethernet interface;CAN bus interface;Odometer interface × 1;Altimeter interface;

Speedometer interface;

Size

335×200×146mm

Weight

<12kg



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