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Brand Name : KACISE
Model Number : KSINS004C
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 : <2mil
KSINS004C Fiber Optic Strapdown Inertial Navigation System
Product Introduction
The KSINS004C fiber optic gyro strapdown navigation system is based on a universal fiber optic inertial navigation platform. The platform adopts a universal design concept and is easy to make adaptive changes according to user needs. It has the advantages of short development cycle, high maturity and good reliability. ; Its supporting gyroscopes, accelerometers, circuits and other components are all made from our existing shelf products, which are mature and reliable.
Feature
● Using domestic fiber optic gyroscope and quartz flexible accelerometer
● The bias stability of type 70 fiber optic gyroscope is better than 0.05°/h (1σ)
● Accelerometer bias stability is better than 50µg (1σ)
● Compatible with static and dynamic base alignment methods, self-alignment and transfer alignment can be selected according to user needs
● Can integrate navigation with external information such as satellite navigation instrument, speedometer, odometer, altimeter, etc., with strong scalability.
Application
●  Land Use
●  Marine Navigation
●  Drones

Technical Specifications
|   Parameter  |    KSINS004C  |  |
|   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  |    <2mil  |  |
|   Circular Error Probable(CEP)  |    <0.1m  |  |
|   Velocity Accuracy  |    <1m/s  |  |
|   Alignment Time  |    <5min  |  |
|   Gyroscope  |    Bias stability  |    ≤ 0.03°/h;≤ 100μg  |  
|   Bias repeatability  |    ≤ 0.03°/h;≤ 50μg  |  |
|   scale factor temperature sensitivity  |    30ppm;50ppm  |  |
|   Random walk  |    ≤ 0.002°/√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/RS-232 × 2;Ethernet interface;Built-in satellite receiver (optional);Odometer interface;Altimeter interface;Speedometer interface;  |  |
|   Size  |    190×150×140mm  |  |
|   Weight  |    <4kg  |  |
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                        KSINS004C Fiber Optic Inertial Navigation System 18-32VDC <20W Images |