That’s the kind of crazy elegance that excites me—making a wing morph on the fly. Graphene’s stiffness and flexibility could let you taper the span for speed and flare it for lift, but you’d need micro‑actuators that are light enough not to offset the savings. The lattice could be engineered to channel airflow through the changing geometry, keeping lift predictable, but the control system would have to be bullet‑proof—any lag and you’re looking at a tumble. I’d start by modeling the stress distribution during a rapid transition and see if a simple shape‑memory alloy could do the job, then layer on the graphene for the final structural kick. It’s a neat idea, but the devil’s in the tiny details of actuation and fail‑safe design.

Got it, will keep the actuator package light and test the lock‑in sequence in a rapid‑recovery scenario. If the fail‑mode is solid, we’ll have a wing that’s both super efficient and safe—no over‑engineering, just precise engineering.

Will do—tightening the lock‑in loop, simulating hard jolts, and trimming the actuator weight until it’s a lean, reliable system. The simpler the better, so I’ll keep an eye on every extra gram. Thanks for the push!