06.2 - Flight Dynamics and Control (UAV related)
TETHERED HOVER FLIGHT TESTS OF BASELINE CONTROL LAWS FOR A TANDEM TILT-WING SUB-SCALE DEMONSTRATOR
D. Milz¹, L. Ott¹, M. May¹; ¹German Aerospace Center (DLR), Germany
A hybrid NDI control law for tandem tilt-wing aircraft is adapted for tethered hover flight tests of a sub-scale demonstrator. The control system and test setup are derived and validating in a structured test campaign. The results allow to infer control performance and robustness (disturbance rejection) for the hover flight.
DOI: 10.71945/icas2026_0404