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FOG Integrated Navigation System

Product description

 

NEW SPACECRAFT FIELD

FOG Integrated Navigation System

FOG Integrated Navigation System, composed of 3 FOGs and 3 quartz accelerometers, has the function of strap-down computation and integrated navigation, featured with high reliability and high precision, which can be used for navigation in the fields of aviation, aerospace and voyage, etc.

 

Qualification

Unit

Parameter

Gyro

Measurement range

(°)/s

> ±60

Threshold

(°)/h

< 0.02

Zero Bias Stability

(°)/h

< 0.02

Bias Repeatability

(°)/h

< 0.02

Scale Factor Nonlinearity

ppm

< 20

Scale Factor Asymmetry

ppm

< 50

Accelerometer

Measurement range

g

±12

Zero Bias Stability

g

< 2.0×10-5

Bias Repeatability

g

< 3.7×10-5

Scale Factor Asymmetry

-

< 1.5×10-4

Scale Factor Repeatability

ppm

< 37

Navigation Precision

/

1Nm/hr

Consumption

W

Steady state:40W,
Startup:100W

Mass

kg

10

Operation temperature range

-40~50

Vibration

grms

11.7

Shock

g

700

Interface

 

RS-422/1553B

 

 

Corresponding parameter set not found, please add it in property template of background
暂未实现,敬请期待
暂未实现,敬请期待
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FOG Integrated Navigation System