An automated method for influencing a gust load of an aircraft is provided. A torque at least of an electromotive thrust generating unit arranged on a wing of the aircraft is modified such that a root bending torque of the wing generated by the gust load is reduced. An associated apparatus, an aircraft, a computer program product, and a computer-readable medium for carrying out the method are also provided.
Gust load reduction in an aircraft
06.02.2024
Patent
Elektronische Ressource
Englisch
Gust Load Alleviation Control for Very Flexible Aircraft
British Library Conference Proceedings | 2011
|"Robust Gust Load Alleviation for a Flexible Aircraft"
British Library Conference Proceedings | 2000
|Gust Load Alleviation Control for Very Flexible Aircraft
AIAA | 2011
|Gust Load Alleviation Control for Very Flexible Aircraft
British Library Conference Proceedings | 2011
|