logo
producten
DETAILS VAN DE PRODUCTEN
Huis > Producten >
Gyrocompass Kalman Filter Fiber Optic Inertial Navigation System FOG INS Half Sine Wave

Gyrocompass Kalman Filter Fiber Optic Inertial Navigation System FOG INS Half Sine Wave

MOQ: 1 set
Prijs: $1000-$100000
Leveringstermijn: 30 werkdagen
Betalingswijze: T/T
Toeleveringskapaciteit: 500 stuks per jaar
Gedetailleerde informatie
Plaats van herkomst
China
Merknaam
Star & Inertia Technology
Lijntijd:
≤5min
Positiegewogenheid/pure traagheid:
≤ 2 nm/1 uur
Positiegewogenheid/Inertiële satellietnavigatie combinatie:
Beter dan satelliet nauwkeurigheid
Snelheidsnauwkeurigheid/pure traagheid:
≤ 1,5 m/s
Snelheidsnavigatie/Inertiële navigatie via satelliet:
≤ 0,2 m/s
Koersnauwkeurigheid/pure traagheid:
≤ 0,1°sec ((L)
Combinatie van koersnavigatie/satellietnavigatie:
≤0,05°
Pitch & Roll nauwkeurigheid/pure traagheid:
≤ 0,03°
Pitch & Roll Accuracy/satellietnavigatie combinatie:
≤ 0,02°
Afmetingen:
130 × 130 × 110 mm
Gewicht:
< 2,2 kg
Temperatuur:
-40 ℃ ~ 60 ℃
Ingangsspanning:
DC24V ((± 25%)
Markeren:

RS422 Fiber Optic Inertial Navigation System

,

ODM Fiber Optic Inertial Navigation System

,

Half sine wave fog ins

Productbeschrijving

The fiber-optic inertial navigation system (FOG INS) integrates a fiber-optic gyroscope with quartz accelerometers in a strapdown configuration and uses high-speed navigation algorithms to output real-time inertial data. The system supports inertial/GNSS integrated navigation and fully autonomous inertial modes, enabling reliable navigation performance in both GPS-available and GPS-denied environments.


Designed for marine and vessel platforms, the system delivers precise heading, roll, pitch, speed, and position outputs to meet the requirements of naval ships, commercial vessels, USVs, and other maritime applications.


Accelerometer Months Bias Repeatability() 30μg
Months Scale Factor Accuracy() 30ppm
Gyro Bias Repeatability() ≤0.01°/hr
Scale Factor Accuracy() 30ppm
Random walk() ≤0.005°/√hr
Features Position Accuracy Pure inertia 2nm/1h,CEP
Inertial navigation satellite combination better than satellite accuracy
Speed Accuracy Pure inertia 1.5m/s,RMS
Inertial navigation satellite combination 0.2m/s,RMS
Angular Rate ≥±400°/sec
Angular Acceleration 100000°/sec2
Acceleration >25g
Angular Attitude  Any Orientation
Input/output 3 RS422 full-duplex serial ports, 1 100M Ethernet port
Alignment time <5min
AHRS Applications Performance Heading Accuracy Pure inertia 0.1°sec(L),RMS
Satellite navigation combination 0.05°,RMS
Pitch & Roll Accuracy Pure inertia 0.03°,RMS
Satellite navigation combination 0.02°,RMS
Characteristics Power consumption <15W
Dimensions 130×130×110
Weight <2.2kg
Temperature  -40℃~60℃
Shock 15g,Half-sine wave 11ms
Input Voltage DC24V(±25%)
cooling Conduction to mounting plate
Vibration  20~2000Hz,6.06g
MTBF >20000 hours



producten
DETAILS VAN DE PRODUCTEN
Gyrocompass Kalman Filter Fiber Optic Inertial Navigation System FOG INS Half Sine Wave
MOQ: 1 set
Prijs: $1000-$100000
Leveringstermijn: 30 werkdagen
Betalingswijze: T/T
Toeleveringskapaciteit: 500 stuks per jaar
Gedetailleerde informatie
Plaats van herkomst
China
Merknaam
Star & Inertia Technology
Lijntijd:
≤5min
Positiegewogenheid/pure traagheid:
≤ 2 nm/1 uur
Positiegewogenheid/Inertiële satellietnavigatie combinatie:
Beter dan satelliet nauwkeurigheid
Snelheidsnauwkeurigheid/pure traagheid:
≤ 1,5 m/s
Snelheidsnavigatie/Inertiële navigatie via satelliet:
≤ 0,2 m/s
Koersnauwkeurigheid/pure traagheid:
≤ 0,1°sec ((L)
Combinatie van koersnavigatie/satellietnavigatie:
≤0,05°
Pitch & Roll nauwkeurigheid/pure traagheid:
≤ 0,03°
Pitch & Roll Accuracy/satellietnavigatie combinatie:
≤ 0,02°
Afmetingen:
130 × 130 × 110 mm
Gewicht:
< 2,2 kg
Temperatuur:
-40 ℃ ~ 60 ℃
Ingangsspanning:
DC24V ((± 25%)
Min. bestelaantal:
1 set
Prijs:
$1000-$100000
Levertijd:
30 werkdagen
Betalingscondities:
T/T
Levering vermogen:
500 stuks per jaar
Markeren

RS422 Fiber Optic Inertial Navigation System

,

ODM Fiber Optic Inertial Navigation System

,

Half sine wave fog ins

Productbeschrijving

The fiber-optic inertial navigation system (FOG INS) integrates a fiber-optic gyroscope with quartz accelerometers in a strapdown configuration and uses high-speed navigation algorithms to output real-time inertial data. The system supports inertial/GNSS integrated navigation and fully autonomous inertial modes, enabling reliable navigation performance in both GPS-available and GPS-denied environments.


Designed for marine and vessel platforms, the system delivers precise heading, roll, pitch, speed, and position outputs to meet the requirements of naval ships, commercial vessels, USVs, and other maritime applications.


Accelerometer Months Bias Repeatability() 30μg
Months Scale Factor Accuracy() 30ppm
Gyro Bias Repeatability() ≤0.01°/hr
Scale Factor Accuracy() 30ppm
Random walk() ≤0.005°/√hr
Features Position Accuracy Pure inertia 2nm/1h,CEP
Inertial navigation satellite combination better than satellite accuracy
Speed Accuracy Pure inertia 1.5m/s,RMS
Inertial navigation satellite combination 0.2m/s,RMS
Angular Rate ≥±400°/sec
Angular Acceleration 100000°/sec2
Acceleration >25g
Angular Attitude  Any Orientation
Input/output 3 RS422 full-duplex serial ports, 1 100M Ethernet port
Alignment time <5min
AHRS Applications Performance Heading Accuracy Pure inertia 0.1°sec(L),RMS
Satellite navigation combination 0.05°,RMS
Pitch & Roll Accuracy Pure inertia 0.03°,RMS
Satellite navigation combination 0.02°,RMS
Characteristics Power consumption <15W
Dimensions 130×130×110
Weight <2.2kg
Temperature  -40℃~60℃
Shock 15g,Half-sine wave 11ms
Input Voltage DC24V(±25%)
cooling Conduction to mounting plate
Vibration  20~2000Hz,6.06g
MTBF >20000 hours



Sitemap |  Privacybeleid | De Goede Kwaliteit van China Lasersysteem voor traagheidsnavigatie Leverancier. Copyright © 2025-2026 CSSC Star&Inertia Technology co.,ltd. . Alle rechten voorbehoudena.