CPC B64C 19/02 (2013.01) [B64C 13/04 (2013.01)] | 18 Claims |
1. A system for distributed pilot control of an aircraft, the system comprising:
a plurality of flight components;
an aircraft control located within the aircraft; and
an aircraft component attached to a flight component of the plurality of flight components, wherein the aircraft component is configured to:
receive, from a command sensor attached to the aircraft control, an aircraft command;
obtain, from an attitude sensor, an aircraft orientation; and
receive, as a function of a notification unit, a pilot signal; and
command the flight component to produce a response command as a function of the pilot signal, wherein producing the response command further comprises:
determining at least an aircraft response, wherein determining at least an aircraft response further comprises:
simulating an aircraft command adjustment as a function of a control algorithm; and
determining the aircraft response using the aircraft command adjustment; and
producing the response command as a function of the aircraft response.
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