Topic Author
Posts: 135
Joined: Mon Apr 23, 2001 7:33 pm


Thu Aug 16, 2001 7:30 pm

Hi folks, does anybody know how that attitude heading reference system works?
I know it includes an atitude heading reference unit made up of two flexdisc gyrometers(haven't a clue of what they are) and of three accelerometers(same as above).
Thanks DIego

RE: Ahrs

Fri Aug 17, 2001 1:20 am

Like the name suggest, the system provides Heading and attitude info to the aircraft ADI and HSI. You can view the AHRS as an integrated VG/DG system or a poor-man IRS. The flexdisc gyrometers you mentioned must be specific to the AHRS you are thinking of.

Basically a typical AHRS contains 2 (or 3) gyroscopes, 3-accelerometers. A gyro picks up rotation perpendicular to its (spin) axis. Each accelerometer picks up acceleration (change in velocity) along its axis. It can detect the earth gravitational field. Together these info are processed by the AHRS computer to give you aircraft attitude (pitch, roll, yaw) and Heading. For magnetic information, flux valves used to be really popular but they are now mostly replaced by magnetic variation tables that computers applied to computed true headings to get magnetic headings.
Posts: 1066
Joined: Fri Mar 16, 2007 1:29 pm

RE: Ahrs

Fri Aug 17, 2001 2:07 am

For the last 20 years, the mechanical gyros have been developed into ring laser units which of course have no moving parts. The accuracy of these devices is astounding.

Best Regards,

Posts: 235
Joined: Fri Jun 01, 2001 8:37 pm

RE: Ahrs

Fri Aug 17, 2001 2:33 am

Try to see on Honeywell's website


Ciao Diego!


Who is online

Users browsing this forum: Rishul93 and 24 guests