IT-AUTOFLIGHT: Difference between revisions

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The roll/yaw modes used by the autopilot.
The roll/yaw modes used by the autopilot.


;HDG (0)
* HDG: A set heading is being tracked. The behavior of the mode can be heading select or heading hold based on pilot selection and user configurable behavior.
A set heading is being tracked. The behavior of the mode can be heading select or heading hold based on pilot selection and user configurable behavior.
* LNAV: A GPS route is being tracked.
 
* LOC: A VOR or ILS localizer is being tracked.
;LNAV (1)
* ALGN: The aircraft is being aligned with the runway for autolands.
A GPS route is being tracked.
* RLOU: Crosswind aileron is applied, and the rudder is used to keep the aircraft on the centerline during rollout.
 
* T/O: A takeoff heading is being tracked, or the wings are being kept level, based on user configurable behavior.
;LOC (2)
* ROLL: A set bank angle is being held.
A VOR or ILS localizer is being tracked.
 
;ALGN (4)
The aircraft is being aligned with the runway for Autolands.
 
;RLOU (4)
Crosswind aileron is applied, and the rudder is used to keep the aircraft on the centerline during rollout.
 
;T/O (5)
A takeoff heading is being tracked, or the wings are being kept level, based on user configurable behavior.
 
;ROLL (6)
A set bank angle is being held.


=== Vertical Modes ===
=== Vertical Modes ===
The pitch modes used by the autopilot. Automatic Pitch Trim is also used.
The pitch modes used by the autopilot. Automatic Pitch Trim is also used.


;ALT HLD (0)
* ALT HLD: Altitude is being held.
Altitude is being held.
* ALT CAP: The pre-selected altitude is being captured.
 
* V/S: A set vertical speed is being tracked.
;ALT CAP (0)
* G/S: A glideslope is being tracked.
The pre-selected altitude is being captured.
* SPD CLB: A set indicated airspeed or mach number is being held by varying pitch angle in order to climb. The autothrottle is commanded to hold the thrust limit.
 
* SPD DES: A set indicated airspeed or mach number is being held by varying pitch angle in order to descend. The autothrottle is commanded to hold idle thrust.
;V/S (1)
* FPA: A set flight path angle is being tracked.
A set vertical speed is being tracked.
* FLARE: The aircraft is being flared for touchdown during an autoland.
 
* ROLLOUT: The nose is lowered at a user configurable rate and then held on the ground via light forward pressure during rollout.
;G/S (2)
* T/O CLB: The takeoff speed (should be set to V2+10 by the aircraft) is being held by varying pitch angle. The autothrottle is commanded to hold the thrust limit.
A glideslope is being tracked.
* G/A CLB: The set go around speed (takeoff speed or current speed, whichever is higher) is being held by varying pitch angle. The autothrottle is commanded to hold the thrust limit.
 
* PITCH: A set pitch angle is being held.
;SPD CLB (4)
A set indicated airspeed or mach number is being held by varying pitch angle in order to climb. The autothrottle is commanded to hold the thrust limit.
 
;SPD DES (4)
A set indicated airspeed or mach number is being held by varying pitch angle in order to descend. The autothrottle is commanded to hold idle thrust.
 
;FPA (5)
A set flight path angle is being tracked.
 
;FLARE (6)
The aircraft is being flared for touchdown during an autoland.
 
;ROLLOUT (6)
The nose is lowered at a user configurable rate and then held on the ground via light forward pressure during rollout.
 
;T/O CLB (7)
The takeoff speed (should be set to V2+10 by the aircraft) is being held by varying pitch angle. The autothrottle is commanded to hold the thrust limit.
 
;G/A CLB (7)
The set go around speed (takeoff speed or current speed, whichever is higher) is being held by varying pitch angle. The autothrottle is commanded to hold the thrust limit.
 
;PITCH (8)
A set pitch angle is being held.


=== Throttle Modes ===
=== Throttle Modes ===
The modes used by the autothrottle. Autothrottle modes are coupled to the vertical modes.
The modes used by the autothrottle. Autothrottle modes are coupled to the vertical modes.


;SPEED (0)
* SPEED: The throttles are driven to maintain a set indicated airspeed.
The throttles are driven to maintain a set indicated airspeed.
* MACH: The throttles are driven to maintain a set mach number.
 
* IDLE: The throttles are slowly driven to the idle stop for speed on pitch descends.
;MACH (0)
* RETARD: The throttles are slowly driven to the idle stop for when under a user configurable radio altitude for the landing flare. On touchdown, they are driven to the idle stop at a faster speed.
The throttles are driven to maintain a set mach number.
* THR LIM: The throttles are slowly driven to the thrust limit for speed on pitch climbs. In takeoff or go around modes, the throttles are driven to the thrust limit at a faster speed.
 
;IDLE (1)
The throttles are slowly driven to the idle stop for speed on pitch descends.
 
;RETARD (1)
The throttles are slowly driven to the idle stop for when under a user configurable radio altitude for the landing flare. On touchdown, they are driven to the idle stop at a faster speed.
 
;THR LIM (2)
The throttles are slowly driven to the thrust limit for speed on pitch climbs. In takeoff or go around modes, the throttles are driven to the thrust limit at a faster speed.


== Installation Instructions ==
== Installation Instructions ==
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