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Strange strong pitch down moment with NOE/A engaged and collective down-low torque


Go to solution Solved by bradmick,

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Posted

From the docs...  Is this what  you are experiencing?  Down Stab would cause a pitch forward with forward airspeed, I would think.

(begin excerpt)
NOE/A. Activates FMC nap of earth/approach mode. In NOE/approach mode, the horizontal stabilator is commanded to 25° trailing edge down when airspeed is below 80 knots. This provides better over-the-nose visibility for low-altitude flying.
(end excerpt)

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Posted

When you go below 80kts the stabilator will schedule down to improve forward visibility, this is normal and expected behavior. This is also why I don’t like the NOE Approach mode. Manual stabilator is the preferred method IMO because you control it, and not the computer and you can better adjust the controls to control the pitch down that happens when the stabilator schedules.

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Posted (edited)

I know it pitchs down below 80kts. That is expected behaviour. Unexpected is that cyclic do not have on some occasions enough authority when you have collective full down to overcome pitch down moment from stabilizator. 

Edited by DeMonteur
Posted
7 minutes ago, DeMonteur said:

I know it pitchs down below 80kts. That is expected behaviour. Unexpected is that cyclic do not have on some occasions enough authority when you have collective full down to overcome pitch down moment from stabilizator. 

 

If you trim the cyclic way forward with the trimmer, it will actually limit how much aft travel you have available. It may be necessary to initially pull it back a ways, retrim, then pull back more. This can be easily observed in the controls overlay RCTRL+ENTER. Pull it up, then add full forward cyclic on the ground and retrim. now pull full aft and see how far the controls indicator moves.

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Posted (edited)
1 hour ago, DeMonteur said:

I know it pitchs down below 80kts. That is expected behaviour. Unexpected is that cyclic do not have on some occasions enough authority when you have collective full down to overcome pitch down moment from stabilizator. 

A rotor system's ability to change the attitude of a helicopter is proportional to how much total thrust it is producing. Redirecting this force vector relative to the center of gravity using the cyclic allows a helicopter to change it's attitude. At low power settings, you can still alter the attitude of the aircraft, but it may take substantially more input due to the weaker force vector.

The stabilator is on the very end of a long moment arm, so even though it isn't a very large control surface, the aggressive deflection of this surface at the end of a long moment arm just below 80 knots can provide quite the force to counter with very little collective application. Even during a normal approach at lower airspeeds, slewing the stabilator trailing edge down requires a fair amount of aft cyclic adjustment to compensate. At 80 knots, you're really on the edge of the controllability envelope with a low power setting.

I mean, the flight model is still work in progress along with everything else, but you're really pushing the intended use under these conditions.

Edited by Raptor9
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Afterburners are for wussies...hang around the battlefield and dodge tracers like a man.
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Posted
9 hours ago, tech_op2000 said:

If you trim the cyclic way forward with the trimmer, it will actually limit how much aft travel you have available. It may be necessary to initially pull it back a ways, retrim, then pull back more. This can be easily observed in the controls overlay RCTRL+ENTER. Pull it up, then add full forward cyclic on the ground and retrim. now pull full aft and see how far the controls indicator moves.

I checked it with ctrl+Enter. I am just writing that even with full aft deflection on control overlay panel and full aft deflection with cyclic with low colective under 80kts I was unable to compensate the pitch down moment from stabilizator. You are then beyond the range of controllability.  I find this behavior dangerous even for combat helicopter. Thats why I fill bugreport with tracks. 

Way to reproduce is turn on NOE/A mode in normal flight around 100kts. Then slow down with full collective down and under 80kts you are unable to compensate pitch down moment even with full aft cyclic.  

  • 2 weeks later...
Posted

I checked NOE/A mode on and reducing airspeed below 80 kts with low collective. At exactly 80 kts the AC‘s nose was diving down really hard.
I was only able to recover because I was prepared what should happen applying full aft cyclic and pull collective…...interesting experience flying in VR……

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Posted (edited)

The main issue I have with NOE/A is that in multi crew it likes to randomly enable itself even when neither crew has selected it from the utility page.

I have had this happen probably 15 to 20 times as a pilot with a human CPG and another 15 or 20 as a CPG for another pilot.

It usually results in near death but most times we recover.

Unless this mode is supposed to enable itself automatically as some kind of brake check style awareness test lol. If so then it seems to be working as intended.

If not then we have another desync bug to report.

Edited by NeMoGas
Posted

It will only enable itself automatically if you select it on, on the UTIL page with the other FMC items. So if during run up someone is toggling it on (the circle is filled in) that’ll do it. Otherwise it doesn’t just come on. I’ve never once had it come on unless I’ve toggled it on. By default it is off on the UTIL page and has to be manually turned on.

Posted

Yeah I figured it would have to be manually turned on. I even check during startup to make sure it is off. Then at some point during the flight I will drop below 80 and the nose will pitch down. I then have to stabilize the helicopter and go into the UTIL page to turn it off. 

My CPG tells me he didn't touch it. I have also seen the same issue when I was CPG and I know I didn't turn it on. 😅

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