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
2020-11-10
Patent
Electronic Resource
English
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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