Products

F-06 Optical Fiber Combined Navigation System

  • Capable of measuring the carrier’s motion angular rate and linear acceleration information.
  • Capable of performing self-inspection of the equipment and outputting self-inspection information.
  • Capable of performing ground self-alignment and air transfer alignment.
  • Capable of performing “pure inertial” navigation and “inertial + satellite” combined navigation.
  • Capable of receiving primary inertial information and sending navigation information through the communication port.
  • Supports online software upgrades.

F-06 Optical Fiber Combined Navigation System

Specifications

Indicators Performance Notes

Gyroscope Performance

Gyroscope zero bias stability ≤0.1°/h 1σ, full temperature range
Gyroscope zero bias repeatability ≤0.1°/h 1σ, full temperature range
Angular rate range -500°/s to +500°/s
Angle random walk ≤0.01°/h<sup>1/2</sup> 1σ, full temperature range
Scale factor nonlinearity ≤100ppm
Scale factor repeatability ≤100ppm
Measurement bandwidth 300Hz phase lag ≤45°, amplitude attenuation ≤-3dB
Startup time ≤10s

Accelerometer Performance

Accelerometer zero bias stability ≤50ug 1σ, full temperature range
Accelerometer zero bias repeatability ≤50ug 1σ, full temperature range
Measurement range -25g to 25g
Measurement bandwidth 500Hz phase lag ≤45°, amplitude attenuation ≤-3dB
Self-inspection time ≤10s

Alignment Method and Time

Alignment method Transfer alignment (using primary inertial or satellite navigation information)
Ground self-alignment
Transfer alignment time ≤3min
Ground self-alignment time ≤5min

Transfer Alignment Accuracy

Heading angle ≤0.05°
Pitch angle ≤0.02°
Roll angle ≤0.02° 1σ, Ground self-alignment
Heading angle ≤0.3°
Pitch angle ≤0.02°
Roll angle ≤0.02°

Navigation Information Update Rate

Navigation information update rate 200Hz configurable

Measurement Range

Pitch angle measurement range -89.5° to +89.5°
Roll angle measurement range -180° to +180°
Heading angle measurement range 0° to 360°

Dynamic Combined Navigation Accuracy (During transfer alignment with maneuvering)

Pitch angle ≤0.02°
Roll angle ≤0.02°
Heading angle ≤0.05°
Horizontal position accuracy ≤5m
Height accuracy ≤10m
Horizontal speed accuracy ≤0.1m/s
Vertical speed accuracy ≤0.1m/s

Combined Navigation to Pure Inertial Navigation Accuracy

Pitch angle ≤0.1° within 20min
Roll angle ≤0.1° within 20min
Heading angle ≤0.1° within 20min
Horizontal positioning hold accuracy ≤2 nautical miles/20min CEP50

Physical and Environmental Requirements

Operating temperature -40°C to +60°C
Storage temperature -50°C to +70°C
Operating Voltage DC18V to 36V ripple ≤200mV
Maximum instantaneous power consumption at startup <40W
Stable power consumption <20W
Startup current <1.5A
Steady-state current <0.6A
Pulse Waveform Acceleration Peak Duration Velocity Change Time Between Successive Shocks ms Shock Direction Number of Shocks
Rear peak sawtooth wave 20 g 11 ms 1.10 m/s ≥55 ms Three axes, six directions 3 times per direction

Composition

The F-06 optical fiber combined navigation system consists of three parts: the fiber optic inertial measurement unit (IMU), the secondary power board, and the navigation computer.

 

Diagram

INS manufacturer

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