yes adapt this wing as if it was an atosTo transform this curved delta wing into a safe, controllable, and high-performing rigid-wing hang glider like an A-I-R ATOS, we must replace weight-shift control with mechanical control surfaces. We also need to fix its stability and low-speed lift.Here is exactly how you would adapt this specific curved shape to match the engineering blueprint of an ATOS rigid wing.1. Structural Transformation: Carbon Fiber D-BoxThe original design appears to be a thick, uniform lifting body. To make it a viable foot-launched glider, you must rebuild the internal structure.Rigid Leading Edge: Build a rigid carbon fiber “D-box” shell along that sweeping, curved leading edge to maintain a perfect aerodynamic airfoil shape under load.Internal Ribs: Run lightweight carbon fiber ribs rearward from the D-box to support a high-tech laminate sail fabric, keeping the wing incredibly light (under 100 lbs / 45 kg) for foot launching.2. Aerodynamic Fixes: Washout and Airfoil ProfileThe original highly swept, low-aspect profile creates massive high-speed drag and low-speed stall risks.Spanwise Twist (Washout): You must twist the wing aerodynamically. Twist the radically swept, curved wingtips so they have a lower angle of attack than the center section. This ensures the center stalls first, keeping the tips flying and preventing a deadly nose-dive tumble.Low-Speed Camber: Replace the supersonic-style airfoil with a high-lift, low-speed profile. The front of the wing must be thicker and rounded to generate high lift at 20–40 mph, rather than needing an engine to get airborne.3. Flight Controls: Implementation of ElevonsBecause this rigid, curved structure cannot be twisted or warped by a pilot’s body weight, you must install mechanical control surfaces along the trailing edge, just like an ATOS.Full-Span Elevons: Split the trailing edge into mechanical flaps called elevons.Control Cable Linkage: Run control cables from these surfaces down to a traditional hang glider A-frame control bar.How it Flies: When the pilot pushes the control bar forward or back, the elevons move together as elevators to pitch the nose up or down. When the pilot moves the bar left or right, the elevons move differentially (one up, one down) to roll the glider into a turn.4. Roll Assistance: Add SpoilersBecause of the heavy sweep and curved shape of this specific wing, it will naturally want to resist rolling into turns (high roll damping).Top-Surface Spoilers: Install small, mechanical spoiler flaps on the top surface of the outer wing panels.Adverse Yaw Correction: When the pilot moves the control bar to turn left, the left spoiler pops up into the airflow. This destroys lift on the left wing and drags it backward, forcing the heavy, curved wing into a smooth, coordinated turn without slipping.Expected Performance of the Adapted WingOnce adapted with ATOS technology, this wing would transform from a dangerous lifting-body concept into a high-performance cross-country glider. It would offer a glide ratio exceeding 19:1, allow for tight thermalling in mountain air, and maintain perfect pitch stability at both high and low speeds.If you would like to explore further, we can look at schematics of how the ATOS control bar hooks up to the spoilers, or look into the exact takeoff and landing speeds required for a rigid wing of this shape. How would you like to proceed?