in an aircraft flight control system, an electric system.reducing the load on the wing in a manaeuvreby comparing the lateral roll, roll up, x) with a threshold (x%)the control and filtering. the action on the control plates.it is possible to predict the load increases due towing and reduce it. the charges may be belowthe maximum value of a design of the aircraft, in the case of controlroll too important compared to the intended use of the aircraft, andto reduce the excessive size of the canopy.
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