Editing Attitude and heading reference system

{{Short description|Sensors providing attitude information on aircraft}}
{{redirect|AHRS|the Alaska survey|Alaska Heritage Resources Survey}}

[[File:Primary_Flight_Display_Garmin_G1000.jpg | thumb | right | alt=Garmin G1000 Primary Flight Display. | Garmin G1000 Primary Flight Display.]]
An '''attitude and heading reference system''' ('''AHRS''') consists of sensors on three axes that provide [[Aircraft attitude|attitude]] information for aircraft, including [[Aircraft principal axes#Longitudinal axis (roll)|roll]], [[Aircraft principal axes#Transverse axis (pitch)|pitch]], and [[Aircraft principal axes#Vertical axis (yaw)|yaw]]. These are sometimes referred to as '''MARG''' (Magnetic, Angular Rate, and Gravity)<ref>{{Cite web|url=http://projectproto.blogspot.de/2011/02/marg-sensors-bluetooth.html|title = MARG sensors + Bluetooth|date = 3 February 2011}}</ref> sensors and consist of either solid-state or [[microelectromechanical systems]] (MEMS) [[gyroscopes]], [[accelerometers]] and [[magnetometers]]. They are designed to replace traditional mechanical [[gyroscopic]] [[flight instruments]].<ref>{{Cite web |title=How It Works: Attitude and Heading Reference System - FLYING Magazine |last=Whitfield |first=Bethany |work=FLYING Magazine |date=16 September 2016 |access-date=15 August 2023 |url= https://www.flyingmag.com/how-it-works-attitude-and-heading-reference-system/}}</ref>

The main difference between an [[Inertial measurement unit]] (IMU) and an AHRS is the addition of an on-board processing system in an AHRS, which provides attitude and heading information. This is in contrast to an IMU, which delivers sensor data to an additional device that computes attitude and heading. With [[sensor fusion]], drift from the gyroscopes integration is compensated for by reference vectors, namely gravity, and the [[Earth's magnetic field]].<ref>{{Cite web|url=https://www.xsens.com/tags/ahrs/|title=AHRS Attitude Heading Reference System|website=Xsens 3D motion tracking|language=en-US|access-date=2019-01-22}}</ref> This results in a drift-free orientation, making an AHRS a more cost effective solution than conventional high-grade IMUs that only integrate gyroscopes and rely on a high bias stability of the gyroscopes.
In addition to attitude determination an AHRS may also form part of an [[inertial navigation system]]. 

A form of non-linear estimation such as an [[Extended Kalman filter]] is typically used to compute the solution from these multiple sources.<ref>[http://wiki.openpilot.org/display/Doc/OpenPilot+Documentation#OpenPilot AHRS – OpenPilot Project<!-- Bot generated title -->]  {{webarchive|url=https://web.archive.org/web/20110812032846/http://wiki.openpilot.org/display/Doc/OpenPilot%2BDocumentation |date=August 12, 2011 }}</ref>

AHRS is reliable and is common in commercial and business aircraft. AHRS is typically integrated with [[electronic flight instrument system]]s (EFIS) which are the central part of [[glass cockpit]]s, to form the primary flight display. AHRS can be combined with [[air data computers]] to form an Air data, attitude and heading reference system (ADAHRS), which provide additional information such as airspeed, altitude and outside air temperature.

==See also==
*[[Acronyms and abbreviations in avionics]]
==References==
{{reflist}}

{{Flight instruments}}

[[Category:Aircraft instruments]]
[[Category:Avionics]]