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Optical Gyroscope Inertial Navigation System For Aircraft Mounted Ship Mounted

Optical Gyroscope Inertial Navigation System For Aircraft Mounted Ship Mounted

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-FINS60S
Applications:
Aerospace, Marine Navigation, Autonomous Vehicles, Military
Navigation Type:
Inertial Navigation
Protection Level:
IP65
Physical Dimensions:
≤140mm×125mm×126mm
User Mode:
Vehicle-mounted (default), Aircraft-mounted, Ship-mounted
Supply Voltage:
24V DC Rated(12~32V DC)
Highlight:

Optical Gyroscope Inertial Navigation System

,

Ship Mounted Inertial Navigation System

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Aircraft Mounted INS Guidance 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 ≤0.04° (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)  

 

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: ≤0.1°sec (Φ) (1σ, Φ is local latitude)
Horizontal attitude alignment accuracy: ≤0.006° (1σ)
Azimuth hold accuracy: 0.02°/h (1σ)
Horizontal Attitude Holding Accuracy: 0.02°/h (1σ)

 

Position Accuracy

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

Speed accuracy

Horizontal speed accuracy: ≤0.8m/s (1σ).

Main Device Characteristics

Gyroscope

range

±500°/s

Zero Bias Stability

≤0.08°/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

4 serial ports (RS232 or RS422)

Support PPS, EVENTMARK input/output

Power Consumption

≤15W

Operating Temperature

-40℃~+55℃

Transmission Rate

9600~961200bps(configurable)

Protection level

IP65

User Mode

Physical Dimensions

≤140mm×125mm×126mm 

 

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

 

 

Weight

≤2.75Kg

Optical Gyroscope Inertial Navigation System For Aircraft Mounted Ship Mounted 0