There's no assumption.Please don’t assume all have had Phantoms Meta.
It was a very pertinent comment since that's when DJI introduced the offset motors.
There's no assumption.Please don’t assume all have had Phantoms Meta.
Thank you, that was a challenging but informative read. I gather now that this is about stability.Lookup 'Dihedral'
The purpose of dihedral effect is to contribute stability in the pitch and roll axis of a Multirotor.
This <link> explains it in scientific words.
As i said he might not have ever had a phantom so he wouldn't know.There's no assumption.
It was a very pertinent comment since that's when DJI introduced the offset motors.
So like I saidBut surely you knew that?
Yes.However, when I look head-on at my Mavic Air, I see the rotors are tilted down and away. This would be an anhedral angle, or a positive βi value, and as such decrease the Mavic Air's (roll) stability, while increasing its maneuverability.
Have I grasped this correctly?
I'm curious to know the brand and model number of the drone in your video.Here is a good flight.. real quick, and pilot avoided VRS!
Thanks for this info! I really did not know about maintaining horizontal motion to smooth out the descent. Now that you mentioned it, I recall all of the combat air missions where we were choppered into an LZ and how much easier it was for the pilot to land when there was room to bring it in at an angle rather than straight down. Some of those chopper pilots were incredible. Almost like parallel parking the chopper into a really tight LZ. Thanks again!I don't own a Phantom.
I can, however, fly a helicopter, and we usually call it Settling with Power. And yes, I know what it is.
What I don't see is how tilting the rotors slightly would alleviate it.
There are three elements to this phenomenon, and all three must be present for it to occur:
I'm not seeing how the slight angling of the downwash would do anything significant to alter any of these factors.
- The rotor is generating sufficient downward thrust
- The vehicle has a significant rate of descent
- The rotor disc has insufficient horizontal motion to be in Effective Translational Lift (ETL)
I've noted that the DJI software limits the rate of descent the pilot can command to a value noticeably less than what you can command for climb. That strikes me as the most effective preventative action against settling with power as it eliminates factor #2.
That said, if you wish to take extra steps to ensure you avoid it, simply maintain a good horizontal component to your speed when coming down.
And if you are descending straight down, and get into the phenomenon, the correct procedure to escape it is to reduce downward thrust (alleviate factor #1), and apply cyclic in any direction (alleviate factor #3). In a helicopter, that usually means forward (most efficient and usually safest direction), but in a quadcopter I don't think it would matter. It is simply that the quickest way to clear the vortex is to move horizontally.
The numbers for rate of descent and ETL depend on the aircraft -- I could tell you what they are for R-22 and R-44 helicopters, but I have no idea what they are for our drones. But ETL occurs essentially by definition from the minimum (or greater) horizontal speed necessary to prevent settling with power.
What I'd like to know is why angling the thrust vector slightly inwards on drones makes a difference. If anyone has information on that, I'd appreciate it.
Thanks for this. It not only added to my understanding of motor tilt, it was an awesome project those guys did as well. It really was impressive looking in flight, and had a motion that seemed to fit perfectly with its scale. I've subscribed to their channel -- they are talented guys.7 minutes into THIS could help understanding motor tilt.
Hopefully the link should start at the correct place.
On my Air there is a full 1/4" difference in hight from one side of the blade to the other when you lay the body on a flat surface.Interesting. I've got an Air, and as far as I can tell, they are straight up and down when viewed side on.
Do you know why they are angled at all? Is it stability?
Right, but they don't tilt fore and aft. I'm guessing this suggests they expect forward flight most of the time?On my Air there is a full 1/4" difference in hight from one side of the blade to the other when you lay the body on a flat surface.
The extended legs are what's angled, so straight on they are level. The 20mm difference may just be in the weight distribution??Right, but they don't tilt fore and aft. I'm guessing this suggests they expect forward flight most of the time?
Had you noticed that their geometry is 20mm wider side-to-side than fore-aft. I wonder what that's about...
Take the same photo but turn the blades 90 degrees looking straight down them. Yes the motors have the tilt, but the blades are now even, or level with each other.Yes, but...
View attachment 90290
Straight-on, you can clearly see the angle of the motor axes, and therefore the rotors. You mentioned this in your first post, so I'm afraid I don't get where you are going with this. Sorry.
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