| Sign In | Join Free | My insurersguide.com |
|
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 | |
|
|
KSINS004C Fiber Optic Inertial Navigation System 18-32VDC <20W Images |