Jioptik F623 F623 Optical Fiber Inertial Integrated Navigation System adopts a strapdown technology solution and advanced data fusion algorithms to provide high-precision and high stability attitude, position, velocity and other information.
● Positioning accuracy(CEP)
● Pure inertia:≤6nm/h
● Course accuracy(RMS)
● Pure inertia:0.5°secL
● Attitude accuracy (RMS)
● Pure inertia:0.3°
● Speed accuracy (RMS)
● Pure inertia:1.5m/s
The STA-F623 inertial measurement unit adopts strapdown technology scheme to provide navigation information such as heading, attitude, speed, position and motion measurement information for the carrier, and can work in combination with systems such as satellite guide, odometer and odometer. Can independently analyze external information and work in the best navigation mode; It has the functions of self-diagnosis of system state and fault state.
F623 Optical Fiber Inertial Integrated Navigation System is suitable for aviation, ground vehicles, surface and underwater navigation, attitude control and other fields.
Project | Indicator | |
Model | STA-F623 | |
Initial alignment time | ≤10min | |
Positioning accuracy(CEP) | Pure inertia | ≤6nm/h |
Inertia/DVL combination | Better than 3%D | |
Inertia/Satellite combination | Better than satellite navigation accuracy | |
Course accuracy(RMS) | Pure inertia | 0.5°secL |
Inertia/Satellite combination | 0.06° | |
Attitude accuracy (RMS) | Pure inertia | 0.3° |
Inertia/Satellite combination | 0.03° | |
Speed accuracy (RMS) | Pure inertia | 1.5m/s |
Inertia/Satellite combination | 0.1m/s | |
Electrical characteristic | Voltage | 20~32V(DC) |
Power consumption in steady state | ≤13W | |
Structural characteristic | Size | ≤110mm×110mm×100mm |
Weight | ≤1.7kg | |
Operating environment | Operating temperature | -40℃~+60℃ |
Storage temperature | 55℃~+70℃ |
Note: All performance indicators and interfaces of fiber optic gyroscope can be customized according to needs.
For more information on our products, please contact Jioptik.