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Kalman Filter GNSS Strapdown Aircraft Inertial Navigation System FOG INS SMALL
Kalman Filter GNSS Strapdown Aircraft Inertial Navigation System FOG INS SMALL
Specifications
Brand Name :
Star & Inertia Technology
Place of Origin :
China
MOQ :
1 set
Price :
$1000-$100000
Payment Terms :
T/T
Supply Ability :
500 sets per year
Delivery Time :
30 work days
Alignment time :
≤5min
Position accuracy/Pure inertia :
5m/60s(Ref.),150m/300s(Ref.),CEP
Position accuracy/Inertial navigation satellite combination :
better than satellite accuracy
Speed ​​accuracy/Pure inertia :
——
Speed ​​accuracy/Inertial navigation satellite combination :
≤0.2m/s
Heading Accuracy/Pure inertia :
≤0.5°secL+0.1°/h,RMS
Heading Accuracy/Satellite navigation combination :
≤0.3°
Pitch & Roll Accuracy/Pure inertia :
≤0.1°
Pitch & Roll Accuracy/Satellite navigation combination :
≤0.05°
Dimensions :
100×100×90mm
Weight :
＜1.5kg
Temperature :
-40℃~60℃
Input Voltage :
DC24V(±25%)
Description

Delivering exceptional navigation performance, this fiber-optic inertial navigation system (FOG INS) integrates FOG/RLG gyroscopes and quartz accelerometers in a strapdown configuration. Its real-time sensor fusion engine combines inertial data with GNSS, celestial, and other navigation sources, ensuring accurate and reliable positioning even in GPS-denied environments.

Key Advantages for UAV Applications

  1. Reliable ground and air alignment for rapid mission readiness

  2. Multiple alignment mode selection for flexible deployment

  3. Scalable navigation augmentation with multi-source integration

  4. Continuous system monitoring for enhanced operational reliability

Series

FOG INS
Accelerometer Months Bias Repeatability(1σ) ≤100μg
Months Scale Factor Accuracy(1σ) ≤100ppm
Gyro Bias Repeatability(1σ) ≤0.05°/hr
Scale Factor Accuracy(1σ) ≤100ppm
Random walk(1σ) ≤0.02°/√hr
Features Position Accuracy Pure inertia 5m/60s(Ref.),150m/300s(Ref.),CEP
Inertial navigation satellite combination better than satellite accuracy
Speed Accuracy Pure inertia ——
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 ≤0.5°secL+0.1°/h,RMS
Satellite navigation combination ≤0.3°,RMS
Pitch & Roll Accuracy Pure inertia ≤0.1°,RMS
Satellite navigation combination ≤0.05°,RMS
Characteristics Power consumption ＜15W
Dimensions 100×100×90
Weight ＜1.5kg
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


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Kalman Filter GNSS Strapdown Aircraft Inertial Navigation System FOG INS SMALL

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Product Detail
Brand Name :
Star & Inertia Technology
Place of Origin :
China
MOQ :
1 set
Price :
$1000-$100000
Payment Terms :
T/T
Supply Ability :
500 sets per year
Contact Supplier
Kalman Filter GNSS Strapdown Aircraft Inertial Navigation System FOG INS SMALL

CSSC Star&Inertia Technology co.,ltd.

Verified Supplier
2 Years
hubei, wuhan
Since 2013
Business Type :
Manufacturer
Main Products :
Laser Inertial Navigation System, Fiber Optic Inertial Navigation System, Aircraft Inertial Navigation System
Total Annual :
5000000-10000000
Employee Number :
300~500
Certification Level :
Verified Supplier
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