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INS Inertial Navigation System For UAV Navigation And Positioning Systems SI-FINS90S
INS Inertial Navigation System For UAV Navigation And Positioning Systems SI-FINS90S
Specifications
Brand Name :
SI
Model Number :
SI-FINS90S
MOQ :
1set
Payment Terms :
D/A,L/C,D/P,T/T,Western Union
Delivery Time :
6-8 weeks
Heading :
≤0.02° (1σ)
Speed accuracy :
Horizontal speed accuracy: ≤0.8m/s (1σ).
Product name :
Fiber Optic Inertial Navigation System
Type :
Inertial Navigation System
Attitude :
≤0.005°(1σ)
Physical Dimensions :
≤170mm×148mm×164mm
Zero Bias Stability :
≤0.01°/H
Description

The SI-FINS90S is an autonomous fixed inertial navigation system. It offers various configuration interfaces and can access external GPS modes, whether they are built-in or external. TJ-FINS90S can be integrated with Hexin Xingtong UM982 . The GNSS receiver has multiple channels (up to 220). The main function of the multi-frequency receiver is to calculate the speed and position of the system and guarantee accurate time (PVT). The receiver has abundant frequency points and can support GPS L1/L2/L5, BDS B1I/B2I/B3I, and GLONASS G1/G2 signals.
The SI-FINS90S can provide the following input interfaces to correct inertial instrument errors:
- Occupancy meter (DMI)
- Doppler Velocimeter (DVL)
- Barometric altimeter
- GPS can also be accessed through the serial interface

Main technical parameters

System Real-time Accuracy

Attitude Accuracy

Heading ≤0.02° (1σ);
Pitch and roll: ≤0.005° (1σ)

Position Accuracy

Single-point horizontal positioning: ≤1.5m (1σ)
Single-point vertical positioning: ≤2.5m (1σ)
RTK level positioning: ≤1cm + 1ppm (1σ)
RTK vertical positioning: ≤2cm + 1ppm (1σ)

Speed Accuracy

Horizontal velocity ≤0.03 m/s (1σ), vertical velocity ≤0.05 m/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: 0.01°/h (1σ)
Horizontal Attitude Holding Accuracy: 0.005°/h (1σ)

Position Accuracy

Positioning accuracy: ≤0.8nmile/h(50%CEP)

Speed accuracy

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

Main Device Characteristics

Gyroscope

range

±300°/s

Zero Bias Stability
≤0.01°/h(1σ, 10s smooth)

Accelerometer

range

±15g

Zero Bias Stability
≤10μg(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

≤170mm×148mm×164mm

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

Weight

≤4.6Kg

INS Inertial Navigation System For UAV Navigation And Positioning Systems SI-FINS90S

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INS Inertial Navigation System For UAV Navigation And Positioning Systems SI-FINS90S

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Product Detail
Brand Name :
SI
Model Number :
SI-FINS90S
MOQ :
1set
Payment Terms :
D/A,L/C,D/P,T/T,Western Union
Delivery Time :
6-8 weeks
Heading :
≤0.02° (1σ)
Contact Supplier
INS Inertial Navigation System For UAV Navigation And Positioning Systems SI-FINS90S

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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