The invention relates to an automated method for influencing a gust load of an aircraft (6), wherein the torque (MI) at least of an electromotive thrust generating unit (1) arranged on a wing (4) of the aircraft (6) is modified such that the root bending torque (M2) of the wing (4) generated by the gust load is reduced. The invention also relates to an associated apparatus and an aircraft and a computer program product and a computer-readable medium for carrying out the method.
GUST LOAD REDUCTION IN AN AIRCRAFT
07.10.2021
Patent
Elektronische Ressource
Englisch
Gust Load Alleviation Control for Very Flexible Aircraft
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|Gust Load Alleviation Control for Very Flexible Aircraft
British Library Conference Proceedings | 2011
|