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High Precision Fiber Optic Gyro INS IF4050 – 0.5° secφ North Seeking

High Precision Fiber Optic Gyro INS IF4050 – 0.5° secφ North Seeking

IF4050 fiber optic inertial navigation system is mainly composed of miniaturized fiber optic gyroscope, MEMS accelerometer, satellite navigation module, main processing board, etc. It has the characteristics of small size, light weight, and low cost, and is suitable for various applications such as small and medium-sized unmanned aerial vehicles, electro-optical pods, underwater robots, etc. The main features are as follows:

→  Automatic North Finding with an accuracy of up to 0.5 °

→  Multiple working modes including pure inertia, inertia/satellite combination, inertia/DVL combination, inertia/mileage combination, inertia/vision combination, and marine compass

→  Automatic North Finding, transfer alignment, satellite assisted dynamic base alignment, high-precision post-processing, and other functions

→  Built in multiple communication protocols, both serial port baud rate and output protocol can be configured

→  Working temperature: -45℃ ~ +70 ℃

→  Equipped with multiple interfaces such as RS422, RS232, Ethernet, PPS input/output, etc

→  Power supply: 12V~36V, power consumption <12W

→  Weight: 0.65kg

 

→  Size: 80mm × 80mm × 70mm

 

  • Número de pieza, :

    IF4050
  • Pedido (MOQ) :

    1
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  • DESCRIPCIÓN

Product Series and Parameters

Parameter Key Performance Indicators
Heading alignment accuracy(1σ) 0.05°( Static dual antenna 2m baseline or single antenna carrier maneuvering)

 0.5(Automatic North Finding)
Attitude alignment accuracy 0.06°(1σ,Automatic North Finding),
0.02°(1σ,Moving base)
Heading Keeping Accuracy 0.3°/h(Pure inertia)
0.1°/h(Combination, extreme situation)
Attitude Keeping Accuracy(RMS) 0.1°(Pure inertia)
0.02°(Satellite combination)
Velocity Accuracy(RMS) 0.02m/s (RMS, Integrated Navigation, Platform Velocity < 500 m/s)
5m/s(Pure inertia)
Position accuracy(CEP) Horizontal < 1.5 m, Vertical < 3 m (RMS, Single-Point
 Positioning, Good Signal Conditions)
Horizontal: < 1 cm + 1 ppm , Vertical: < 2 cm + 1 ppm ( RMS,  Satellite-based Carrier Phase Differential; Link Condition: Good)
6nmile/h(Pure inertia)
Alignment Time 4.5 minutes (Automatic North Finding), 1 minute (Dual antenna assisted
 orientation), 15 minutes (Moving base)
Gyroscope Range 500°/s
Zero bias stability 0.2°/h(10s Smoothing)
Resolution 0.01°/h
Bandwidth 400Hz
Accelerometer Range 40g
Zero bias stability 200ug
Operating Temperature -45℃~70℃
Interface Power and communication socket model J30J-31ZK, with interfaces including RS422, RS232, Ethernet, PPS output/input, and customizable CAN interface
The antenna is SMA × 2
Data rate Navigation data: up to 200Hz, IMU data: up to 1kHz
Power supply Rated 24V DC, can adapt to 12V~36V
Power consumption <10W
Dimension 80mm×80mm×70mm(Excluding socket and mounting bracket)
Weight About 0.65kg

Production process


Product dimension

FOG INS

 


Application Scenarios

FOG INS application
The FOG-based INS (Inertial Navigation System) is suitable for high-accuracy navigation and guidance scenarios such as UAV/VTOL and aircraft navigation, vehicle/ship attitude & heading reference and GNSS/INS integrated navigation, antenna/radar/electro-optical stabilization platforms, and survey-grade mobile mapping & georeferencing—delivering ultra-low drift, excellent bias stability, and strong vibration/EMI robustness for long-duration and demanding environments.
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MEMS accelerometer for UAV
UAV
MEMS accelerometer for robots
Robots
MEMS accelerometers are used in autonomous driving
Autonomous Driving

FAQ

1. What are the primary application scenarios for the IF4050 Inertial Navigation System?
The IF4050 is a high-precision inertial navigation system based on fiber-optic gyroscopes. Characterized by its compact size and lightweight design (weighing only 0.65 kg), it is suitable for various unmanned platforms—including small to medium-sized UAVs, electro-optical pods, and underwater robots—and is particularly well-suited for applications with stringent requirements regarding both navigation accuracy and weight reduction.
 
2. What is the heading alignment accuracy of the IF4050?
Static dual-antenna (2m baseline) or single-antenna maneuvering alignment: 0.05°
Self-north-seeking accuracy: 0.5° × secφ (latitude-corrected)
 
3. What is the attitude alignment accuracy?
In self-north-seeking mode: 0.06°
Moving-base alignment: 0.02°
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