One embodiment is an aircraft including at least one propulsion assembly; a cargo area for receiving payload to be transported by the aircraft; and a control system for determining characteristics of the received payload; automatically determining optimal control gains for operating the aircraft including the payload based on the determined payload characteristics; and providing control signals to at least one of the at least one propulsion assembly and a control assembly of the aircraft to control operation of the at least one propulsion assembly in accordance with the determined optimal control gains.
ADAPTIVE FLIGHT CONTROLS
14.05.2020
Patent
Elektronische Ressource
Englisch
Online Contents | 1994
|NTRS | 1982
|SAE Technical Papers | 1970
|British Library Online Contents | 2007
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