FPDM61-MEMS Inertial Navigation System

FPDM61-MEMS Inertial Navigation System

High accuracy dual antenna GPS/INS fusion Attitude Measurement System

Description

FPDM61 is a high accuracy dual antenna GPS/INS fusion attitude measurement system. It uses GPS carrier measurement technology, information fusion technology to obtain high-precision positioning, orientation, attitude information, which can be widely used in various areas such as aircraft, ships, vehicle dynamic measurement and it can also be used for high precision fast timing, positioning, orientation, attitude measurement and other fields of antennas, pods, photographic equipment.

 

Specification

Position Accuracy

Level Accuracy(RMS)

2m

Altitude Accuracy(RMS)

4m

Attitude Accuracy

Heading Accuracy(RMS)

0.3°(Baseline≥1m)

Attitude Accuracy(RMS)

0.3°

Speed Accuracy

 

0.2°/s

GPS Index

Main Performance

16 Parallel Channels; L1; Acceleration: 4g;

Vibration: 7.7g; Time Service Accuracy(1pps): 50ns

Maximum Speed

515m/s

Maximum Altitude

18000m

Gyro Index

Type

MEMS

Measuring Range

90°/s

Bias

0.2°/s

Bias Stability

10°/h

Scale Factor Repeatability

1000ppm

Scale Factor Non Linearity

1000ppm

Accelerometer Index

Type

MEMS

Measuring Range

2g

Bias

2mg

Bias Stability

0.5mg

Scale Factor Repeatability

1000ppm

Start Time

 

500ms

Data Frequency

 

100Hz

Interface Feature

Interface Type

RS232/RS422(Output)

Baud Rate

9600~115200bps

Electric Performance

Working Voltage

12VDC Rated(12V~36VDC)

Power Consumption Typical Value

5W

Physical Feature

Dimensions

147×85×75mm

Weight

1000g

Environmental Feature

Operating Temperature

-40℃~65℃

Storage Temperature

-50℃~85℃

 

Features

Small volume, low power consumption, high reliability, and stable performance.

 

Applications

It is suitable for applications of small volume and high precision heading attitude control and stable platform.

 

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