I’ve been asked to help out with this problem.
The user is building a fixed wing with v-tail. They noticed that the “rudder-elevator” servo deflection is much greater in yaw than it is in pitch
I don’t know what flight mode was used for the test. I’ve not built a v-tail, but my guess is that in MANUAL flight node, there should be full “rudder-elevator” servo deflection for both pitch and yaw.
Am I correct about this assumption?
Perhaps if the user was in a FLY BY WIRE mode, the difference in pitch and yaw deflection might exist.
Would someone please offer some suggestions on understanding why the rudder-elevator servos deflect less in pitch than in yaw.
Thank you!