Aircraft, flight control device and method for determining maneuvering reserve in aircraft

A method for determining a maneuvering reserve in an aircraft having a number of propulsion units, preferably a multirotor VTOL aircraft, most preferably an aircraft with electrically operated drive units for the rotors, includes the steps: determining a control vector [tau]=(L M N F)T for the aircr...

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Bibliographische Detailangaben
Hauptverfasser: SEIFERTH CHRISTOPH, STEFAN JOCHEN
Format: Patent
Sprache:chi ; eng
Schlagworte:
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