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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
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
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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Fiber Optic Inertial Navigation System KSINS002C 18-32VDC Images |