公开(公告)号：US20180015997A1

公开(公告)日：2018-01-18

申请号：US15209105

申请日：2016-07-13

申请人： Embraer S.A.

发明人： Gustavo Jose ZAMBRANO ,  Tiago Francisco Gomes DA COSTA ,  Fernando Antonio PAVÃO

IPC分类号： B64C13/16 ,  B64C25/50 ,  B64C25/42 ,  B64C25/34 ,  B60T8/17 ,  B64D45/00 ,  B60T7/04

CPC分类号： B64C13/16 ,  B60T7/042 ,  B60T8/1703 ,  B60T8/18 ,  B60T8/325 ,  B60T2230/03 ,  B60T2230/04 ,  B64C25/34 ,  B64C25/42 ,  B64C25/50 ,  B64D45/00

摘要： A flight control law enhances braking efficiency through the operation of aircraft elevators (or another pitch control system) using measured longitudinal acceleration and/or pedal position as references to the control law. Through this solution, it is possible to increase the vertical load in the main landing gear and consequently enhance braking efficiency.