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UAVs Ships Inertial Navigation System Navigation Vehicles INS System SI-FINS60S

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MEMS Inertial Measurement Unit [5]
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Single Axis Gyroscope [12]
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UAVs Ships Inertial Navigation System Navigation Vehicles INS System SI-FINS60S

Brand Name : SI

Model Number : SI-FINS60S

MOQ : 1set

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

Delivery Time : 6-8 weeks

Bias Stability : ≤0.08°/h

Pitch and roll : ≤0.01° (1σ)

Applications : Aerospace, marine navigation, autonomous vehicles, military

Navigation Type : Inertial Navigation

Heading : ≤0.04° (1σ)

Physical Dimensions : ≤140mm×125mm×126mm

User Mode : Vehicle-mounted (default), aircraft-mounted, ship-mounted

Supply voltage : 24V DC rated(12～32V DC)

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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

UAVs Ships Inertial Navigation System Navigation Vehicles INS System SI-FINS60S

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UAVs Ships Inertial Navigation System Navigation Vehicles INS System SI-FINS60S

UAVs Ships Inertial Navigation System Navigation Vehicles INS System SI-FINS60S

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