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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Format: | Patent |
Sprache: | chi ; eng |
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