VTOL tuning high yaw gains and ground oscillations with vectored tilt Quicktune LUA

Hi,

first a huge thank you to the creators of the LUA QUICKTUNE script for VTOLS! @tridge @hwurzburg @hendjoshsr71 @Iampete1 @magicrub

This is incredibly helpful and enables us to do an inital tune of our aircraft in a small space with a safety line attached to the aircraft.

We are building a Quadcopter with two big motors on the fuselage and two smaller motors on the wingtip that can be tilted for yaw control. RPM-Yaw control is not possible due to the propeller arrangement.
YAW_Headroom is set to 0.

The Quicktune code brought us a great tune on pitch and roll. On roll it is almost too direct but thats something we can manage and change later.

We do have problems/questions on YAW.

  1. We already started with a P value of 2 from our previous rough manual tuning. With extended values for the LUA script we still reached the limit both on P=3.0 and D=0.5.
    In the air this felt incredibly good on yaw. Finally we had a precise and direct actuation.
    Unfortunately these settings result in heavy oscillations while on the ground.
  2. we manually reduced the values to P=1.6 D = 0.02 → fixed the ground oscillation. But the tune in the air is much worse again.

Does anybody have comparable experience or even a hint how we can approach this better?
Higher I values instead of P/D?

-Christian

edit: we also tried lower P/D values within the suggested limits. It was barely flyable and the quicktune automatically going up to the limits again…

try setting the yaw axis FF term as explained here Tailsitter VTOL Tuning — Plane documentation for a vectored yaw…for vectored yaw FF is sometimes the dominant pid term…then rerun yaw QuikTune

2 Likes

Hardware option. You could consider to tilt/cant the motor angles to increase Yaw.

on vectored yaw, cant has no effect, total throw does…but I doubt that would have impact…its a tuning issue, not max throw issue

thanks a lot!
We didn’t look at FF yet.
Will try as soon as weather gets better.