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Fiber Optic Gyroscope Fog Satellite Integrated Navigation System
  • Fiber Optic Gyroscope Fog Satellite Integrated Navigation SystemFiber Optic Gyroscope Fog Satellite Integrated Navigation System

Fiber Optic Gyroscope Fog Satellite Integrated Navigation System

JIO-F100S fiber optic integrated navigation system is composed of high-precision closed-loop fiber-optic gyroscope, quartz Flexible accelerometer and high-end GNSS receiving board, through multi-sensor fusion and guidance Realization of aerial calculation algorithm, providing high-precision navigation attitude,speed and position information to the outside world information to meet high-precision measurement and control requirements. Welcome to buy Fiber Optic Gyroscope Fog Satellite Integrated Navigation System from us.

Model:JIO-F100S

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Product Description


Fiber Optic Gyroscope Fog Satellite Integrated Navigation System Features

JIO-F100S fiber optic integrated navigation system is composed of high-precision closed-loop fiber-optic gyroscope, quartz Flexible accelerometer and high-end GNSS receiving board, through multi-sensor fusion and guidance Realization of aerial calculation algorithm, providing high-precision navigation attitude,speed and position information to the outside world information to meet high-precision measurement and control requirements.

JIOPTICS installation of fiber optic gyroscope to provide ease of integration flexibility, and our developers toolkit to rapid prototyping, not only meet the specification requirements, also provide high-quality performance meet the demand of end users.

Our services

JIOPTICS is a professional and efficient team. Provide OEM/ODM services for you, contact us to customize your exclusive fiber optical gyroscope

Product Features

- 0.8nmile/h navigation grade accuracy
- Multi-mode selection, vehicle mode/airplane mode
- Static initial alignment 3min / shaking base initial alignment 8min
- Fault self-check
- Rich interfaces, support RS232, RS422, CAN and other standard interfaces
- High reliability

Application scenarios

-Intelligent excavation system in mining area
- Baseline inertial navigation for large UAVs
- marine compass
- self-propelled gun orientation
- Vehicle positioning and orientation
- High precision mobile measurement
- High precision and stable platform

Electrical characteristics

-Delectrical power supply: 24V DC (typical value)
-Reze power: 1.5W (maximum value)
-The ripple: 100mv (peak value)

Electrical Characteristics

- Power supply: 24~36V DC (typ.)
- Rated power: 30W (max)

Mechanical Dimensions



Technical parameters

Attributes
Parameter
Index
Position hold
Odometer Combo
0.001D (D is mileage)
GNSS combination
1.2m
Pure inertia
0.8nmile/h
Attitude accuracy
Initial alignment
0.003°
Attitude hold
(GNSS disabled, pure inertia)
0.002°/10min(RMS)
Transient power
≤100W (<3s)
Heading accuracy
self-seeking north
0.05°×sec(Lati), where Lati means latitude (RMS)
Heading hold
(GNSS disabled, pure inertia)
0.003°/10min(RMS)
Speed accuracy
Speed hold
(GNSS disabled, pure inertia)
0.3m/s/10min(RMS)
Optical fiber Gyro
Measuring range
±400°/s
Zero bias stability
≤0.01°/h
Quartz Flexible Accelerometer
Measuring range
±20g
Zero bias stability
≤20µg(10s average)
Communication Interface
RS232
1 channel (baud rate 9.6kbps~921.6kbps, default 115.2kbps
Frequency up to 1000Hz, default 200Hz)

RS422
6 channels (Baud rate 9.6kbps~921.6kbps, default 115.2Kbps
Frequency up to 1000Hz, default 200Hz)
Structural properties
Size
199 mm × 180 mm × 219.5 mm (L×W×H)
Weight
A single set of inertial navigation is not more than 8.0kg (optional for aviation applications is not more than 6.5kg)
Use environment
Storage temperature
-40℃~65℃
Relative humidity
≤80%



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