| CPC B64C 13/0421 (2018.01) [B64C 13/503 (2013.01); B64C 13/505 (2018.01); B33Y 80/00 (2014.12); B64C 29/0033 (2013.01)] | 20 Claims |

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1. A three-dimensional control assembly for an electric aircraft, the three-dimensional control assembly comprising:
an aircraft frame;
a support structure coupled to the aircraft frame; and
a control stick coupled to the support structure and having:
a length and a radius, wherein the control stick is configured to be manipulated:
along a first axis to control a pitch of the electric aircraft;
along a second axis perpendicular to the first axis to control a roll of the electric aircraft; and
rotationally about the length of the control stick to control a yaw of the electric aircraft, wherein the control stick is further configured such that rotation about the length of the control stick in a first direction changes a yaw of the electric aircraft in the first direction, and rotation about the length of the control stick in a second direction changes a yaw of the electric aircraft in the second direction; and
a linear thrust control disposed adjacent an end of the control stick and including:
a thumbwheel configured to control at least a forward thrust propulsor of the electric aircraft; and
a resistance mechanism configured to change a resistance against movement of the linear thrust control based on a rotational position of the control stick.
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