It was suggested that I test an actual flight and find out, What is Up with Yaw? Generate the data, and then present that to the group. That this would be much more productive than talk. So I set up a test ship and took 208 data points.
I'll be first to admit that physics can be surprising.
I recently put a chain in a box that was raised up on a pedestal. Then I dropped one end of the chain over the edge of the box so that the chain would pull the rest of the chain out of the box. What surprised me was that the chain, rather than slice the wall of the box in two as it ran out of the box, instead looped up and didn't touch the wall of the box. The higher the box was raised off the floor, the higher the chain soured upwards into the air before it was pulled down to the floor. Once I saw this, the reason was obvious. But it certainly was not obvious to me without seeing it first. For your pleasure, here is the video.
Back to yaw. The question the group has been struggling with is:
o Is Yaw force different than thrust force in how it should be treated?
o Is rotor yaw strongest when it's at the center?
My belief was that no. Force is force is force. While counter rotational forces of the motor are created quite differently than thrust forces, it's still a force. But who cares what an old fart like me with dying brain cells thinks? Let's do the damn test!
So here is the graph.
Here is the data
So what does this tell us. It tells us two things:
o first, we can definitely reject the hypothesis that yaw force is strongest when the rotor is at the center of the ship.
o second, my premise might also be wrong, because there appears on the surface to be a slight increase in force as the rotor is moved away from center (remember that my prediction was that the force would not change; force is force is force).
So what's with this 0.3% upward slope? There are two possible causes that my wee brain is aware:
- Twisting the bar so the motor can tilt into yaw. The bar, however, was a 1.5" aluminum extrusion that isn't going to twist enough when subjected to a mere 60 gram force. So that's not a likely candidate.
- Rotor tilt.
We all know how hard it is to create a thrust vector that is perfectly perpendicular to the rotor plane. So could this be it? Did the rotor have a slight lean into the direction of yaw which would generate greater yaw torque the farther the rotor was from the center (same principle of physics when two kids of equal mass sit at different distances from the center of a teeter totter; the kid nearest the center is going to get launched upwards)?
If the bias in slope is caused by a slight rotor tilt, how can one tell? Easy ... fortunately. Just slide the rotor across to the other side of the bar. If it is thrust helping yaw on one end of the bar, on the opposite end, the tile will work against the yaw rotational force.
This is the result of that test.
Bingo. The slope is zero. So nothing surprising to me after all. Darn. I love being surprised like the magic trick above. The 0.3% bias was cause by a 0.34 degree tilt in the rotor. Hey, that's as good as I could get it. And as long as one tests along both ends of the bar, these minor biases can be averaged out.
What was the test procedure? I'm hoping that someone will replicate this test to confirm the data, so we can correct the quad and octa V. So there is a photo of the test setup and my messy mancave (please forgive me, I've been doing a ton of tests on custom mujlti-rotor Vs).
To help move this along, I'm also willing to host someone who is near to Hood River, Oregon, USA. My wife's princess palace has a great suite upstairs. We can repeat the test together.
Note: Force was measured at a constant location on the T-Bar as can be seen in the photo. To derive the correct units of force (versus proportional units), divide all data points by 19.5.
I'll let Leonard and others mull this over. This data proves that:
o rotational force is constant no matter the location on the bar.
o rotational force is no different in treatment to thrust force that is also constant no matter the location along the bar.
o thrust force and rotational force are thus both governed by the same torque law.
o thereby, the APM/3DR is correct in code and procedure. The factors "are set by their coordiantes."
o In the case of yaw, how far the motor is from the z-axis of rotation that goes through CG.***
o When any alternate approach to setting V yaw pitch and roll factors differs from the coordinate framework, we need to talk.
***Caveat: Leonard, there is something that is strange about yaw that someone smart in math like you is needed to solve. I'd like to make the following suggestion. I'm going to friend you so we can work this together offline and come up with a unified approach. Hopefully you will now let me work using geometry to solve for the coordinates of the quad and octa V as stated in 3DR/APM procedure, with your oversight. If you want join with me to do this, I'll share this strange thing about yaw with you that doesn't impact regular ships but does impact some custom ships. It might be nothing, but it also might be something we need to consider that no one else is.
--