One embodiment is an aircraft (100) including at least one propulsion assembly (115); a cargo area (102) for receiving payload to be transported by the aircraft 9100); and a control system (20) for determining characteristics of the received payload; automatically determining optimal control gains for operating the aircraft (100) including the payload based on the determined payload characteristics; and providing control signals to at least one of the at least one propulsion assembly (115)and a control assembly of the aircraft (100)to control operation of the at least one propulsion assembly (115) in accordance with the determined optimal control gains.
ADAPTIVE FLIGHT CONTROLS
ADAPTIVE FLUGSTEUERUNGEN
COMMANDES DE VOL ADAPTATIVES
2023-10-11
Patent
Elektronische Ressource
Englisch
IPC: | B64U |
Online Contents | 1994
|NTRS | 1982
|SAE Technical Papers | 1970
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