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High Precision Fiber Optic INS SI-FINS60S Pure Inertial Index: Horizontal Alignment ≤0.006°(1σ), Azimuth Hold 0.02°/h (1σ), Attitude Hold 0.02°/h (1σ) For UAV, Ship & Unmanned Vehicle Navigation

High Precision Fiber Optic INS SI-FINS60S Pure Inertial Index: Horizontal Alignment ≤0.006°(1σ), Azimuth Hold 0.02°/h (1σ), Attitude Hold 0.02°/h (1σ) For UAV, Ship & Unmanned Vehicle Navigation

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
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)
Highlight:

Optical Gyroscope Inertial Navigation System

,

Ship Mounted Inertial Navigation System

,

Aircraft Mounted INS Guidance System

Product Description

This inertial navigation system integrates a built-in three-axis high-precision fiber optic gyroscope, high-precision quartz flexure accelerometer, and mobile mapping-grade multi-mode multi-frequency GNSS receiver with autonomous BeiDou capability. Powered by advanced intelligent integrated navigation algorithms and Kalman filtering, the system is optimized to mitigate GNSS signal occlusion and multipath interference. It delivers high-precision measurement of heading, attitude, velocity and position for moving carriers.

Equipped with multiple sensor interfaces including GNSS, odometer, DVL and barometric altimeter, the system satisfies long-duration, high-accuracy and high-reliability navigation requirements under complex environments such as urban canyons. It is applicable to navigation and control for a wide range of 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

High Precision Fiber Optic INS SI-FINS60S Pure Inertial Index: Horizontal Alignment ≤0.006°(1σ), Azimuth Hold 0.02°/h (1σ), Attitude Hold 0.02°/h (1σ) For UAV, Ship & Unmanned Vehicle Navigation


Products
PRODUCTS DETAILS
High Precision Fiber Optic INS SI-FINS60S Pure Inertial Index: Horizontal Alignment ≤0.006°(1σ), Azimuth Hold 0.02°/h (1σ), Attitude Hold 0.02°/h (1σ) For UAV, Ship & Unmanned Vehicle Navigation
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
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)
Minimum Order Quantity:
1set
Delivery Time:
6-8 weeks
Payment Terms:
D/A,L/C,D/P,T/T,Western Union
Highlight

Optical Gyroscope Inertial Navigation System

,

Ship Mounted Inertial Navigation System

,

Aircraft Mounted INS Guidance System

Product Description

This inertial navigation system integrates a built-in three-axis high-precision fiber optic gyroscope, high-precision quartz flexure accelerometer, and mobile mapping-grade multi-mode multi-frequency GNSS receiver with autonomous BeiDou capability. Powered by advanced intelligent integrated navigation algorithms and Kalman filtering, the system is optimized to mitigate GNSS signal occlusion and multipath interference. It delivers high-precision measurement of heading, attitude, velocity and position for moving carriers.

Equipped with multiple sensor interfaces including GNSS, odometer, DVL and barometric altimeter, the system satisfies long-duration, high-accuracy and high-reliability navigation requirements under complex environments such as urban canyons. It is applicable to navigation and control for a wide range of 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

High Precision Fiber Optic INS SI-FINS60S Pure Inertial Index: Horizontal Alignment ≤0.006°(1σ), Azimuth Hold 0.02°/h (1σ), Attitude Hold 0.02°/h (1σ) For UAV, Ship & Unmanned Vehicle Navigation