DLR institute Projects

hesham

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Dynamic wind tunnel simulation of a highly augmented flexible model aircraft with canard control surfaces. The test rig and model aircraft demonstrated open- and closed-loop control laws for variable stability functions, rigid body gust alleviation, and elastic mode suppression systems (Project BASE).

http://www.dlr.de/ft/desktopdefault.aspx/tabid-1388/1918_read-3396/
 

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From Lotnictwo 5/2018.
 

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DLR has tested a new morphing wing on its PROTEUS unmanned aircraft, allowing the wing to change shape continuously during flight. The system uses a hyperelastic trailing edge and an AI‑based flight controller to improve efficiency, control, and robustness against failures. Initial flight tests were successful, and larger‑scale trials are planned for 2026.
Sources (German):
https://www.dlr.de/de/aktuelles/nachrichten/2026/dlr-testet-im-flug-verformbaren-fluegelhttps://www.flugrevue.de/flugzeugbau/dlr-projekt-morphair-fluegel-ohne-klappen-und-querruder/
 

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