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High Precision Fiber Optic Gyro Inertial Navigation System Combination For Aircraft

High Precision Fiber Optic Gyro Inertial Navigation System Combination For Aircraft

MOQ: 1set
Delivery Period: 6-8 weeks
Payment Method: D/A,L/C,D/P,T/T,Western Union
Detail Information
Brand Name
SI
Model Number
SI-FINS88S
Productname:
Fiber Optic Inertial Navigation System
Application Fields:
Aerospace, Marine, Land Vehicles
Power Consumption:
Low Power
Driftrate:
Low Drift
Navigationtype:
Inertial Navigation
Updaterate:
Real-time
Weight:
Lightweight
Highlight:

Fiber Optic Gyro Inertial Navigation System

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Precision INS System For Aircraft

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Fiber Optic Gyro INS System

Product Description

This product has built-in three-axis integrated high-precision fiber optic gyro, high-precision quartz flexure accelerometer and mobile mapping grade multi-mode and multi-frequency GNSS receiver supporting autonomous BeiDou function. Through the advanced intelligent combination navigation algorithm and Kalman filter, optimized design for GNSS obstruction and multi-path interference, it can realize high-precision heading, attitude, speed and position measurement of moving carriers.
This inertial navigation system has a variety of sensor interfaces such as GNSS/odometer/DVL/barometric altimeter, which can well meet the needs of long-time, high-precision and high-reliability navigation applications in complex environments such as urban canyons, and can be used for the navigation and control of various unmanned systems.

Main technical parameters

System Real-time Accuracy

Attitude Accuracy

Heading ≤0.05° (1σ); 
Pitch and roll: ≤0.01° (1σ)

Position Accuracy

Single-point positioning: horizontal ≤2m (50% CEP).
RTK: horizontal ≤2cm + 1ppm (50% CEP).

Speed Accuracy

0.02m/s (Carrier speed less than 500m/s)  

Data update rate

400Hz(configurable)

Alignment Time

Start timing after obtaining latitude, longitude and altitude position information. The alignment process duration is ≤5 minutes.

Inertial/ODO/DVL Combination

0.5%×Miles traveled (depending on the accuracy of the external odometer)

Pure Inertial Specification

Attitude Accuracy

Azimuth alignment accuracy: ≤0.5°sec (Φ) (1σ, Φ is local latitude)

Horizontal attitude alignment accuracy: ≤0.01° (1σ)
Azimuth hold accuracy: 0.15°/h (1σ)
Horizontal Attitude Holding Accuracy: 0.1°/h (1σ)

Position Accuracy

Positioning accuracy: ≤1nmile/h(50%CEP)

Main Device Characteristics

Gyroscope

range

±500°/s

Zero Bias Stability

≤0.15°/h(1σ, 10s smooth)

Accelerometer

range

±20g

Zero Bias Stability

≤30μg(1σ, 10s smooth)
 

Physical Characteristic

Interface Characteristics

Supply voltage

24V DC rated(12~32V DC)

Interface method

3 serial ports (RS232 or RS422)

Support PPS, EVENTMARK input/output

Power Consumption

≤14W

Operating Temperature

-40℃~+55℃

Transmission Rate

9600~961200bps(configurable)

Protection level

IP65

User Mode

Physical Dimensions

≤100mm×100mm×120mm 

 

Vehicle-mounted (default), aircraft-mounted, ship-mounted

 

 

Weight

≤1.4Kg

High Precision Fiber Optic Gyro Inertial Navigation System Combination For Aircraft 0