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Fiber Optic INS Guidance System For UAV USV Vehicle Navigation Systems SI-FINS90S-H

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Fiber Optic INS Guidance System For UAV USV Vehicle Navigation Systems SI-FINS90S-H

Brand Name : SI

Model Number : SI-FINS90S-H

MOQ : 1set

Payment Terms : D/A,L/C,D/P,T/T,Western Union

Delivery Time : 6-8 weeks

Sensor technology : Fiber Optic

Navigationtype : Inertial Navigation

Dimensions : ≤170mm×148mm×164mm

Accuracy : High precision

Outputdata : Position, velocity, and attitude information

Protection level : IP65

Power Consumption : ≤25W

Heading : ≤0.015° (1σ)

Attitude : ≤0.005°(1σ)

Zero Bias Stability : ≤0.005°/H

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The SI-FINS90S-H 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-H 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 ≤0.015° (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: ≤0.03°sec (Φ) (1σ, Φ is local latitude) Horizontal attitude alignment accuracy: ≤0.006° (1σ) Azimuth hold accuracy: 0.006°/h (1σ) Horizontal Attitude Holding Accuracy: 0.005°/h (1σ)
Position Accuracy	Positioning accuracy: ≤0.6nmile/h(50%CEP)
Speed accuracy	Horizontal speed accuracy: ≤0.5m/s (1σ).
Main Device Characteristics
Gyroscope	range	±500°/s	Zero Bias Stability		≤0.005°/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

Fiber Optic INS Guidance System For UAV USV Vehicle Navigation Systems SI-FINS90S-H

Product Tags:

Fiber Optic INS Guidance System

Self Contained INS Guidance System

Fiber Optic INS Guidance System For UAV USV Vehicle Navigation Systems SI-FINS90S-H Images

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