But you aren't coordinating it.
Your just dividing your input in half. I always wondered when I watched you fly why your turns had so much yaw movement. Now I know if that much input you use!
The 777 has a Yaw Damper anyways (I think)
It's still an odd way to fly in my opinion.
Mixed auto coordination
Re: Mixed auto coordination
it0uchpods wrote:But you aren't coordinating it. You're just dividing your input in half.
Correct. Hence "auto" coordination. It's a compromise for pilots using the keyboard, mouse or joysticks with jittery twist axes. Not ideal but better than no coordination at all.
I haven't seen an autopilot that implements a yaw damper, but until I tried Richard's Aero VSP FDM for the Beagle Pup, I hadn't experienced dutch roll in a Flightgear FDM either.
Re: Mixed auto coordination
A fair few aircraft have an aileron rudder interconnect (ARI) usually as part of a stability augmentation system (SAS); the F-15 definitely does, some research aircraft (M2F2) had a configurable version of ARI where you can set the gain via a cockpit control. The gain on the F-15 is a function of elevator and flaps (at elevator -24 the gain is -0.9, 0 is -0.105, 15 is 0.406); flaps adds roughly 0.1 to these figures. The F-15 has also got a yaw damper - but this is part of the SAS and can be turned off. You can notice that the yaw damper is off often at M>0.8 where you can get yaw oscillation (it's a feature of the airframe).
The built auto coordination is a very simplistic ARI - it's not a yaw damper.
All of the Boeing 7xx series have a yaw damper; since 1959 when they fitted it to the 707; pretty certain that all of the Airbus have it as well.
It's fairly easy to add an effective yaw damper as it's really just a function on the angular velocity r ; this is the F-15 version.
The built auto coordination is a very simplistic ARI - it's not a yaw damper.
All of the Boeing 7xx series have a yaw damper; since 1959 when they fitted it to the 707; pretty certain that all of the Airbus have it as well.
It's fairly easy to add an effective yaw damper as it's really just a function on the angular velocity r ; this is the F-15 version.
Code: Select all
<scheduled_gain name="fcs/yaw-damper-sum">
<input>velocities/r-aero-rad_sec</input>
<table>
<independentVar>velocities/vc-kts</independentVar>
<tableData>
0 0
80 0
120 3.6251
650 1.65
890 1.00
1000 0.5
</tableData>
</table>
<clipto>
<min>-0.2000</min>
<max>0.2000</max>
</clipto>
</scheduled_gain>
<scheduled_gain name="fcs/yaw-damper-dmd">
<input>fcs/yaw-damper-sum</input>
<table>
<independentVar>aero/qbar-psf</independentVar>
<tableData>
2.9900 0.0000
3.0000 1.0000
</tableData>
</table>
<gain>fcs/yaw-damper-active</gain>
</scheduled_gain>
<summer name="Rudder Sum">
<input>fcs/rudder-command-sum</input>
<input>fcs/yaw-damper-dmd</input>
<clipto>
<min> -1.1 </min>
<max> 1.1 </max>
</clipto>
</summer>
Re: Mixed auto coordination
On my IT autopilots, I now block "auto"coordination while the AP is on, because it causes problems with the roll control. I might end up adding a YD to it using the slip/skid indicator, outputting to rudder, which would engage whenever one or more APs is on.
But I still think autocoord is useless except for taxiing. It might cause issues during flight.
J
But I still think autocoord is useless except for taxiing. It might cause issues during flight.
J
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