# Is it possible to use a plane's entire wing as an elevon?

Would it be feasible to build an RC plane using the entire wing as an elevon, with each wing independently moved up and down with servos? For roll control, they would be moved in opposite directions; for pitch, they would move together. (Of course, in reality, both will be done at once.)

I'm asking here rather than on the drone site because the question is mostly about theory, and this site seems a lot more active than the drone one.

(Obviously not to scale)

Green: Propeller

Red: Movable wings

Yellow: Center of gravity

Blue: Fixed wing

• You mean aileron? If the entire wing is moving differentially, the pitch trimming forces have to come from somewhere else. Jan 30, 2023 at 3:04
• @JohnK I was thinking of moving both wings together for pitch. Would that work? Jan 30, 2023 at 3:10
• If you implement it on a conventional airplane where CG is in front of the wing, pitching the wing up will cause a nose down, which conflicts with the pitch-up of the wing. To make it work, the pivoting wing must be in (near) front of the CG and there needs to be another pair of wings (of similar size) further after the CG to stabilize the pitch. Jan 30, 2023 at 4:13
• @user3528438 something like the diagram I added? Jan 30, 2023 at 4:42
• So from your picture it seems like you are designing a propeller version of an Eurofighter ðŸ˜‰ Do you have also a vertical tailplane? Jan 30, 2023 at 19:41

Would it be feasible to build an RC plane using the entire wing as an elevon, with each wing independently moved up and down with servos?

Yes, such designs exist. They are most often seen in radio-controlled slope gliders. The key is that there is also a horizontal tail which is fixed. Otherwise there would be no pitch control-- moving the wings together in the same direction would accomplish nothing in a tailless design.1

If the wings move in the opposite direction for roll control, but pitch control is accomplished with elevators on the horizontal tail (or with an all-moving horizontal tail), then the design is described as a "wingeron" design. (The term is a "portmanteau" of "wing" and "aileron".) With proper gearing, "wingeron" designs can be built with only one servo driving the wing movement, or two servos can be used.

If the wings move in opposite directions for roll control and also move together for pitch control, as posited by the O.P. here, then the aircraft is described as a "pitcheron" design. This word is "portmanteau" of "pitch" and "wingeron". "Pitcheron" designs always need two servos to control the wings.

Here is a photo of a "Pica" radio-controlled slope-soaring glider-- a "pitcheron" design, with no elevators or other moving parts on the horizontal tail (actually a V-tail in this particular case). (Source: "Slopeflyer" website )

Here is a photo of a Sig "Samurai" radio-controlled slope-soaring glider-- a "wingeron" design, with elevators on the horizontal tail (again, actually a V-tail in this case). (Source: "Wanderings" website.)

Note the absence of ailerons in all the photos.

Here's a link to a YouTube video of a Sig Samurai "wingeron" glider in action. The internal workings are briefly visible near the start of the video. One single servo controls both wings for roll control. One more servo to control the elevator function of the tail would have been sufficient. In this particular case the glider is set up with a second servo for the tail (making three servos in all) to allow the moving surfaces to act as "ruddervators" (as in a Beechcraft Bonanza) rather than just as elevators, but the rudder function is really not necessary in a fast aircraft of this nature, and certainly is not a significant source of roll control, since the wing has neither dihedral nor sweep to create slip-roll coupling. As noted in the video, this particular design is often built with just two servos, omitting the rudder function of the tail surfaces.

Link to a related question on a model airplane discussion forum: Pitcheron & Wingeron. What's the difference?

Note than in the case of a powered aircraft, a "pitcheron" design will create a "thrust vectoring" effect that might be less than optimal, depending on the specific details of the design. When the pilot increases the angle-of-attack of the wing by moving the control stick aft, he is essentially tilting the thrust vector slightly downwards relative to the wing, which seems less than ideal. However, if the thrust line can be configured to pass through or near the CG of the aircraft regardless of wing position, then this is not the same as an increase in "downthrust" angle, which would generally have much a more unfavorable effect on handling. Naturally, you could always consider mounting the motors on the wings.

Finally, note that a key feature that allows the pitcheron or wingeron designs to work well in radio-controlled models is that there is no need to consider the aerodynamic "feel" transmitted from the control surfaces back to the control stick, or the position that the controls will go to if the pilot relaxes all forces on the control stick and just lets the control stick "float" freely. In radio-controlled models, we are only concerned about stick-fixed stability, not stick-free stability. Likewise we are only concerned with the control surface position that must be maintained to obtain a given result, not the force that must be applied to the control system to obtain that result. The situation is very different with full-sized airplanes, at least so long as the control system is "reversible", i.e. so long as aerodynamic forces can be transmitted from the control surfaces back to the control stick or yoke. The same difference also applies to all-moving horizontal or vertical tails-- they are simpler to implement in radio-controlled models than in full-scale aircraft with conventional "reversible" control systems.

Footnotes:

1. Re "moving the wings together in the same direction would accomplish nothing in a tailless design" -- except for hang gliders and other weight-shift-controlled aircraft! The key here, of course, is that if the CG is far enough below the rotation point of the wing (which in a hang glider is essentially the point where the pilot's "hang strap" is attached to the rigid structure of the glider), then rotating the wing (relative to the rest of the aircraft "structure", i.e. the pilot's body, or the "trike" unit in the case of a powered "trike") accomplishes a significant forward or aft translation of the CG of the whole system, relative to the wing.
• Thank you! So as long as I have a fixed tail, it is possible to fly with only two movable surfaces (not counting the propeller)? Jan 30, 2023 at 4:05
• A notable example is AIM-7 Sparrow AA missile. Jan 30, 2023 at 4:08
• Thank you! The Pica looks very similar to the design I'm thinking of. Is the Sig Samurai's tail broken? I only see half of the V. Jan 30, 2023 at 4:48
• It would be nice to find a nice video of the "Pica" in action too, ideally showing a look at the internal linkages, but searching is complicated by the fact that there are apparently at least two rc slope-soarers also called "Pica" that are a much more conventional design, and also an RC flight sim program, and also a paraglider, all with the same name. May put some more effort into it later -- Jan 30, 2023 at 4:51
• @kj7rrv -- see added content re thrust line effects (now re-worked) , and control "reversibility" (last two paragraphs) Jan 30, 2023 at 16:08