Patent ID: 9446837
Filing Date: 2016-09-20
CPC Classification: B64C,B64D,G05D

Claim Text:
1. A method of dynamically alleviating loads generated on an aircraft by a disturbance of gust, the method comprising the steps of: automatically detecting a disturbance due to gust on a flight of the aircraft; automatically generating control commands for control surfaces when a disturbance due to gust is detected; applying the control commands to actuate the control surfaces; dynamically actuating the control surfaces in a prescribed dynamic way in order to minimize both a first load peak and a second load peak; and generating control commands using a predetermined control command sequence that has been pre-determined in a previous control command sequence determining step, wherein the control command sequence determining step comprises: determining the vector of variable θ by optimization calculation such that the load response to the typical wind gust shape is minimized.