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Gyrocompass Kalman Filter Universal Fiber-optic Gyro SINS Strapdown Technology

Gyrocompass Kalman Filter Universal Fiber-optic Gyro SINS Strapdown Technology

MOQ: 1 set
Delivery Period: 30 work days
Supply Capacity: 100 set per year
Detail Information
Place of Origin
China
Brand Name
Star & Inertia Technology
Alignment Time:
≤5min
Position(Pure Inertial):
≤1nm/10min
Position(Satellite Assis):
Better Than Satellite Accuracy
Heading(Pure Inertial):
≤1°sec(L)
Heading(Satellite Assis):
≤1°
Pitch And Roll(Pure Inertial):
≤0.2°
Pitch And Roll(Satellite Assis:
≤0.2°
Speed(Pure Inertial):
/
Speed(Satellite Assist):
0.2m/s
Weight (kg):
<0.5
Environmental Adaptation:
Meet Temperature, Vibration, Electromagnetic And Other Environment Requirements
Power And Interface:
Power Supply DC18V~36V;Digital Outputs With Network Port, RS422 Serial Port, CAN Port, Etc.
Product Description

The fiber-optic inertial navigation system (FOG INS) uses fiber-optic gyroscopes (FOG) and quartz accelerometers as its core sensors, delivering high-precision navigation for a wide range of platforms. Built on strapdown technology and enhanced with advanced real-time navigation algorithms, it continuously outputs accurate position, velocity, heading, and attitude data.

This system supports multiple operational modes, including integrated inertial/satellite navigation and standalone inertial navigation, providing flexible solutions for different mission requirements. Its robust design and high accuracy make it ideal for various vessel platforms, ensuring precise heading, roll, pitch, speed, and position information even in challenging environments.

products
PRODUCTS DETAILS
Gyrocompass Kalman Filter Universal Fiber-optic Gyro SINS Strapdown Technology
MOQ: 1 set
Delivery Period: 30 work days
Supply Capacity: 100 set per year
Detail Information
Place of Origin
China
Brand Name
Star & Inertia Technology
Alignment Time:
≤5min
Position(Pure Inertial):
≤1nm/10min
Position(Satellite Assis):
Better Than Satellite Accuracy
Heading(Pure Inertial):
≤1°sec(L)
Heading(Satellite Assis):
≤1°
Pitch And Roll(Pure Inertial):
≤0.2°
Pitch And Roll(Satellite Assis:
≤0.2°
Speed(Pure Inertial):
/
Speed(Satellite Assist):
0.2m/s
Weight (kg):
<0.5
Environmental Adaptation:
Meet Temperature, Vibration, Electromagnetic And Other Environment Requirements
Power And Interface:
Power Supply DC18V~36V;Digital Outputs With Network Port, RS422 Serial Port, CAN Port, Etc.
Minimum Order Quantity:
1 set
Delivery Time:
30 work days
Supply Ability:
100 set per year
Product Description

The fiber-optic inertial navigation system (FOG INS) uses fiber-optic gyroscopes (FOG) and quartz accelerometers as its core sensors, delivering high-precision navigation for a wide range of platforms. Built on strapdown technology and enhanced with advanced real-time navigation algorithms, it continuously outputs accurate position, velocity, heading, and attitude data.

This system supports multiple operational modes, including integrated inertial/satellite navigation and standalone inertial navigation, providing flexible solutions for different mission requirements. Its robust design and high accuracy make it ideal for various vessel platforms, ensuring precise heading, roll, pitch, speed, and position information even in challenging environments.

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