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Self Contained Fiber Optic Inertial Navigation Vehicles Or Aircraft Mounted SI-FINS75S-H
Self Contained Fiber Optic Inertial Navigation Vehicles Or Aircraft Mounted SI-FINS75S-H
Specifications
Brand Name :
SI
Model Number :
SI-FINS75S-H
MOQ :
1set
Payment Terms :
D/A,L/C,D/P,T/T,Western Union
Delivery Time :
6-8 weeks
Bias Stability :
≤0.015°/h
Attitude :
≤0.005°(1σ)
Heading :
≤0.02° (1σ)
Physical Dimensions :
≤140mm×126mm×136mm
Protection level :
IP65
Operating Temperature :
-40℃~+55℃
Accuracy :
High precision
Type :
Inertial Navigation System
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 ≤0.02° (1σ);
Pitch and roll: ≤0.005° (1σ)

Position Accuracy

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

Speed Accuracy

≤0.03m/s (1σ).

Alignment Time

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

Inertial/ODO/DVL Combination

0.2%×Miles traveled (depending on the accuracy of the external odometer)

Pure Inertial Specification

Attitude Accuracy

Azimuth alignment accuracy: ≤0.05°sec (Φ) (1σ, Φ is local latitude)

Horizontal attitude alignment accuracy: ≤0.006° (1σ)
Azimuth hold accuracy: 0.015°/h (1σ)
Horizontal Attitude Holding Accuracy: 0.006°/h (1σ)

Position Accuracy

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

Speed accuracy

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

Main Device Characteristics

Gyroscope

range

±300°/s

Zero Bias Stability
≤0.015°/h(1σ, 10s smooth)

Accelerometer

range

±15g

Zero Bias Stability
≤20μg(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

≤25W

Operating Temperature

-40℃~+55℃

Transmission Rate

9600～961200bps(configurable)

Protection level

IP65

User Mode

Physical Dimensions

≤140mm×126mm×136mm

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

Weight

≤2.8Kg

Self Contained Fiber Optic Inertial Navigation Vehicles Or Aircraft Mounted SI-FINS75S-H

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Product Detail
Brand Name :
SI
Model Number :
SI-FINS75S-H
MOQ :
1set
Payment Terms :
D/A,L/C,D/P,T/T,Western Union
Delivery Time :
6-8 weeks
Bias Stability :
≤0.015°/h
Contact Supplier
Self Contained Fiber Optic Inertial Navigation Vehicles Or Aircraft Mounted SI-FINS75S-H

Stable Inertial Systems Ltd.

Verified Supplier
1 Years
beijing, beijing
Since 1997
Business Type :
Manufacturer, Seller
Main Products :
MEMS Inertial Measurement Unit, MEMS Inertial Navigation System, Single Axis Gyroscope
Total Annual :
5000000-10000000
Employee Number :
500~1000
Certification Level :
Verified Supplier
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