AHRS-004
    Publish time 2016-09-08 16:27    

It is civil aviation inertial navigation system standards of the new generation of navigation systems and it can effectively protect the flight safety and transport efficiency.

AHRS-004
AHRS-004

Description:

The inertial navigation system of civil aviation carries out differential correction and integrity monitoring to the global satellite navigation system. By measuring the attitude parameters, angular velocity, acceleration information and heading angle of the motion carrier, the magnetic field disturbance and distortion are eliminated to improve heading accuracy.


Product advantages:
1, To provide accurate roll, pitch and heading information;
2, The global satellite navigation correction and monitoring;
3, Sensitive to the magnetic field around the calibration by interference, thereby eliminating magnetic field distortion, improving heading accuracy;

Parameters:

Attributes

Index

Heading

Range

±180°

Accuracy

< 2°

Resolution

0.01°

Attitude

Range: Roll, pitch

±180°

Dynamic Accuracy

<0.3°

Resolution

0.01°

Angular velocity

Range: roll, pitch, yaw

±300°(±900°)

Zero absolute error

< 0.15deg/s(< 0.02deg/s)

Zero - point instability

Resolution

0.01°

ARW

< 0.15°

Acceleration

Range

±6g

Bias stability

< 5mg

Resolution

< 1mg

working environment

Power shock

100g@6ms

Non-power shock

10000g@6ms

Anti-seismic

6g rms

Operating temperature

-40°—85°

Electrical interface

Input voltage

5-13V

Size

84 x 60 x 35mm

Weight

50g

Interface Type

10Pin