An aircraft includes an airframe having an aircraft longitudinal axis and a main rotor system supported by the airframe. The main rotor system is rotatable about an axis of rotation. The airframe is tiltable relative to a ground surface to form a non-zero tilt angle between the aircraft longitudinal axis and the ground surface.
ENHANCED TAXI CONTROL FOR RIGID ROTORS
VERBESSERTE ROLLSTEUERUNG FÜR STARRE ROTOREN
COMMANDE DE ROULAGE TAXI AMÉLIORÉE POUR DES ROTORS RIGIDES
2021-03-10
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
Control issues for rigid-in-plane helicopter rotors
AIAA | 1996
|Control Issues for Rigid-in-Plane Helicopter Rotors
Online Contents | 1996
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