A separated lift-thrust (SLT) aircraft includes a longitudinal-thrust engine and articulated electric rotors, at least some of which are variable-position rotors having variable orientations based on rotor position signals. Control circuitry independently controls thrust of the longitudinal-thrust engine and the thrust and orientation of each of the variable-position rotors, relative to the aircraft lifting surface and longitudinal thrust engine, to provide for commanded thrust-vectoring maneuvering of the aircraft during VTOL, fixed wing flight, and intermediate transitional states, including maintenance of a desired pose of the lifting surface independent of orientation of the rotor orientations when hovering the aircraft in windy conditions. A flight and navigation control system automates flight maneuvers and maintains desired aircraft pose and position relative to static or dynamic coordinates during station keeping, tracking, avoidance, or convergence maneuvers.
SEPARATED LIFT-THRUST VTOL AIRCRAFT WITH ARTICULATED ROTORS
SENKRECHTSTART- UND -LANDEFLUGZEUG MIT GETRENNTEM HUB-SCHUB UND GELENKIGEN ROTOREN
AÉRONEF VTOL À LEVAGE-POUSSÉE SÉPARÉ DOTÉ DE ROTORS ARTICULÉS
2022-06-22
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
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