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Fiber Optic Integrated Navigation System

Fiber Optic Integrated Navigation System

Model: S300D

Short Description:

The fiber optic integrated navigation system S300D is based on cost-effective closed-loop fiber optic gyroscope,accelerometer and high-end GNSS receiving board, through multi-sensor fusion and navigation solution algorithm implementation to meet the needs of medium and high-precision mobile measurement systems, large UAVs, etc.

The application field requires accurate measurement of attitude, heading and position information.


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Technical Parameter

Technical indicators

Product Tags

Product Features

The fiber optic integrated navigation system S300D is based on cost-effective closed-loop fiber optic gyroscope,accelerometer and high-end GNSS receiving board, through multi-sensor fusion and navigation solution algorithm implementation to meet the needs of medium and high-precision mobile measurement systems, large UAVs, etc.

The application field requires accurate measurement of attitude, heading and position information.

Application scenarios

The system has a combined inertial/satellite navigation mode and a pure inertial mode.

The satellites that can be received by the GNSS receiver in the inertial/satellite integrated navigation mode satellite positioning information for combined navigation; output inertial solution position after losing signal speed attitude, with meter-level positioning accuracy in a short time.

After the pure inertia mode is started, it has the function of accurate attitude measurement and can output pitch rolling and heading, pure inertia can statically seek north.

Product Features

- Position accuracy up to centimeter level

- Attitude measurement error better than 0.01°

- Operating temperature range: -40~60℃

- Vibration environment: 20~2000Hz, 3.03g

- Rich interface types, support RS232, RS422, CAN and other standard interfaces

- Mean time between failures up to 30000h

Electrical Characteristics

- Power supply: wide voltage input 12~36V

- Rated power: 24W (max)

Attitude measurement system1

Mechanical Dimensions

Attitude measurement system15
Attitude measurement system16

Technical indicators

Parameter

Attributes

Typical value

Unit

Position accuracy

Single point (RMS)

1.2

m

RTKRMS

2cm+1ppm

 

Post-processing (RMS)

1cm+1ppm

 

Loss of Lock Accuracy (CEP)

2nm①

 

Heading (RMS)

Combined accuracy

0.1②

º

Post-processing

0.01

º

Loss of lock retention accuracy

0.02①

º

North-seeking accuracy

0.2③

ºSecL

 

Attitude (RMS)

Combined accuracy

0.01

º

Post-processing

0.006

º

Loss of lock retention accuracy

0.02①

º

Horizontal Velocity Accuracy (RMS)

 

0.05

m/s

Timing accuracy

 

20

ns

Data output frequency

 

200④

Hz

Gyro

Range

300

º/s

Zero bias stability

0.02⑤

º/h

Scale factor

50

ppm

Corner random walk

0.005

º/√hr

Accelerometer

Range

16

g

 

Zero bias stability

50⑤

μg

Scale factor

50

ppm

Speed random walk

0.01

m/s/√hr

Speed random walk

Parameter

Attributes

Reference

Unit

Physical size

Size

176.8×188.8×117

mm3

 

Weight

< 5

kg

Electrical Characteristics

Rated voltage

12~36

V

Rated power

24 (steady state)

W

Memory

Reserved

 

 

Environmental indicators

Operating temperature

-40~+60

Storage temperature

-45~+70

Random vibration

3.03 20~2000Hz

g

MTBF

30000

h

Interface features

 

PPS, EVENT, RS232, RS422, CAN (optional)

 

 

Network port (reserved), antenna port, wheel speed sensor port

 

Note:

① The alignment is valid, and the lock is lost for 60 minutes;

②Vehicle conditions, need to be maneuvered;

③Two-position alignment, 15min alignment, the difference between the two positions is greater than 90 degrees;

④ Single output 200Hz;

⑤10s average.


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  • Parameter

    Attributes

    Typical value

    Unit

    Position accuracy

    Single point (RMS)

    1.2

    m

    RTK(RMS)

    2cm+1ppm

     

    Post-processing (RMS)

    1cm+1ppm

     

    Loss of Lock Accuracy (CEP)

    2nm①

     

    Heading (RMS)

    Combined accuracy

    0.1②

    º

    Post-processing

    0.01

    º

    Loss of lock retention accuracy

    0.02①

    º

    North-seeking accuracy

    0.2③

    ºSecL

     

    Attitude (RMS)

    Combined accuracy

    0.01

    º

    Post-processing

    0.006

    º

    Loss of lock retention accuracy

    0.02①

    º

    Horizontal Velocity Accuracy (RMS)

     

    0.05

    m/s

    Timing accuracy

     

    20

    ns

    Data output frequency

     

    200④

    Hz

    Gyro

    Range

    300

    º/s

    Zero bias stability

    0.02⑤

    º/h

    Scale factor

    50

    ppm

    Corner random walk

    0.005

    º/√hr

    Accelerometer

    Range

    16

    g

     

    Zero bias stability

    50⑤

    μg

    Scale factor

    50

    ppm

    Speed random walk

    0.01

    m/s/√hr